SCIENTIFIC ABSTRACT ARZHAKOV, S.A. - ARZHANOV, Y.P.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000102320003-0
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 6, 2000
• Sequence Number: 3
• Publication Date: December 31, 1967
• Content Type: SCIENCEAB

ARZHAKOV, S.A.; RTLOV, Tejo.; SHTARDW, B.P.
Pressure sintering of powdered polymers. -Fart 1: Regions where
transparent specimens are obtained. Vysokom. soed. I
no.9:1351-1356
'59 (MIRA 13:3)
~Pblymers) (Methacrylic acid) (Acrylic acid)

AREILUCY, S.A.; RYLOV, Tejo.; SHTARWAN, B.P.
I - ~ I -- ~, -~~ ...
Preseure sintering of powdered polymers. Part 2:
Regions of true
compaction. Vysokom. soed. I no,9;1357-1360 5 '59.
(HIRA 13:3)
(Polymers) (Hathaorylic aoid) (Acrylic acid)

ARZHAKOV, S.A# RTLOV, Te.Te.; SHTARDM, B.P.
Effect of pressure on the Softening temperature of polymers.
Vysokom. soed. 1 no.9-.i438 159. (MIRA 13:3)
(Polymers--Thermal properties)

39576
S/020,/62/145/003/010/013
B101/B144
RS: -,Arzhakov, S Rylov, Ye. Ye., Slonimskiy, G. L., and
Shtark.man, B. P.
Tile role of thormal destruction when molding polymethyl metha-
crylate powder into monolithic solids
PERIODICA'A"; Aknde.niya nauk SSSR. Doklady, v. 145, no, 3,
19062, 595 - 597
Cl~:,K'-: The authors studied the conditions for the production
of molded
specimens of polymethyl :-,.ethacr'ylate (PtIlleA) po,.-.-der
rhich do not lose their
t.,:.,n.r;,j,irency when annealed at a temperature 30 OC abo4e
thevitrifirtion
s:)ecimons were molded at a prc!j.-~urc of 50 kg/cm and a
molding temoerature (t ) of 100 - 2500 C. At t -1350C, the
transparency
Q rl 0 m
decreased linearly after annonline, at- ..-180 C the cpecimen
became opaque.
1 0
The molecular wei,~ht of decreased above 130 C owing to thermal
~Icstri;ction, tnen it reached a mirimur, in the viscous -
liquid state at
170-1600C and increased apin at 190-2300C owing to easier
recombination
of inacroradicals. Above 2300C decomposition of the
macromolecules and
Vard 1/2

S/020/62/145/003/010/013
The role of thermal destruction ... Biol/B144
t4 o, 0
f 0 rm. of &-iocoua i-,iono-mors set in. Between 130 and 190 C,
transparency
with the molecular weight. Conclusions: the loss in trans-
.)arency is a measure for the relaxation of the grains deformed by
moldin-,.
rD
nused by se.)aration of C-C bonds. Hence, increased moldin-
..oiz~zatkon is c V f
or inhibitor addition (0.22-,-., diphenyl picryl hydrdzine) deceler-
ates the relaxation and im-pedes the production of transparent
specimens.
,:GaS.urX..ento4' the decrease in specimen hei&ht durinC annealing
showed that
lo;-,;I-i-.'.hm of the molding time depends linearly on-the
reciprocal
t;_-.7.,~or.,Jure at %,,hich the height becomes constant. The
activation onerCzy
~75 kcal/.-.010) thus calculated, is in good agreement with that of
the C-C
bond. -Perfectly molded specimens are obtained at temperatures and
pressures whkch -oarantee complete relaxation. "here are 4 fituros.
i*..arch 17, 1962, by V. A. Kargin, Academician
114arch 17, 1962
bard 2/2

J,
_AGCESSMN NR: --I
0
AUTHM.- LdbedWv -.IV,4*I 6htArkffAki2`LB ~zbskm S. A.
...........
TIM: Sow ze(~~ pr6bleis -in -the packing
of powder po3pwra
SOURCE: PIA9titibes" mmmyp - nos 69 1963p 32-37
TOPIC TAGS: psaini proiezo of Powder Paymers, porosity-pressure
depanaenoo,
porosity-tempereture dependence
J'ABSTRADT: The 41stribuiion of pressure during the compression of a
number of
der polymars in the pressure interval from 0 to 50D0 %g POW
cm~lsquare am at room tam-
parature has been Investigated. It ban been proven that the proissure
during the
compression of samplen of powder polymers such &9 palyvinylahloride,
polymetbyl-
metaorylate, poIrlsobut7l. ana polyisc=qImetacry'lata, is distributed
accordiM to
tbe expwaential lav. It was shown that the relationship between the
applied
prpsowe and the pressure trapsmitted through th~ sample polymer is
related to the
'properties of tbb compressed powder through a ooofficient of
particle friction on
I the walls of the press and tbroi%b the applied w0ight and the angle
of natural
de4ection. The porosity.de Of the polp, uers on the applied pressure
in them
intervals betweem 0 to 5DOD kg pare am van iaso atutUed. It vas
established
that the pressur) required for the attainment of density equal to the
density of
Card 2/2

'AGGESSION M: APP01581
the particle's of p6);4er material is characteristic for each
individual polymer and
does not do )Dn.thO eha ir if the" temperature is
pond pe,9 size or quantity of powde il .
constants With UO inmlwe of tozparature, the vaguitude of t~o
characteristic
Pressurs dooroas,os~ Comparison of thin dependeMs with the lower
proomro limit
i necessary to'obtiii transparent sazoploB from
pokymethylmetacryla" powder has
proven the point of ~Iev that the presence of thoan limits la
stipulated by the
narrowing of -the particles during the ooWospioxt of powder to the
full limit of
campr4siou of tho',ftpe volume betvm thwA. . :nv uselessness of~
the o~dsting
experimental fbnmxjA used previously in the description of the
porosity dependence I
on the pressure IM''ieen indicated. A new empirical for=Aa which
eatiafactor !
'corresponds with the -experimentra'.datis.bas been. proposede
Orige art, has: 4.
tables, 6 figurosi*
ASSOC IAT IDN t moi ib
ME AGQs OIJuI63 =14 00
SUB CODIgg -OTMS
0 _MW San' 008 002
Card 2/2

L 15603-63 LW(J)/EPF(C)/E'NT(m)/BD1; As D pc-4/pr-4 W
1VW/JW/M1r
ACGESSIOH NRs Anooh7o6 3/0190/63/005/008/1196/1200
F.
AUTHORSs. Arzhakov, S,, A.;, Ry:~lov, Ye. Ye.; Slonimskiy, 0. L.;
Shtarkman, B.._
TITLEt Peculiarities in the formationof monolithic solids under the
effect of
pressure and temperature on polyacrylonitrile powder
SOURCEI Vy*sokomo.*Leku1yarny*ye soyedineniva v*. 5, no, 8, 1963f
1196-1200
TOPIC TAGSs mon6-1:ithic solidi'po2yacrylonitrile,- pressure)
temperature, plastici-- I
zation of' polymer
ABSrRACT i The present investigation was-undertaken to study the
formation of
!transparent monolithic solids from polymeric substances with rigid
chains and
vitrification temperatures neat, or above their decomposition
margin, Polyacryl-
onitrile as such (or plasticized by vapors of dimethylformamido) was
subjected i
to various pressures at a temperature range of 50-2000o When the
state of trans-
parency (estimated b~y visual means) had been reached, the
corresponding pressure
and temperature were recorded and plotted its log P - T. It was
found that trans-
parency in the solid state can be achieved at 140C, providing log P
is 3.5, while
at atmospheric pressure polyacrylonitrile would decompose at 250C
before any
Cord V2

L 1_56o3-63
;ACCESSION HRs AMD4706
j
I vitreous state had been reached. When subjected to compression at
a temperature i
above 150G, powdered polyacrylonitrilo loses itat solubility in
dinet)Wlrormamide,
:except when brought to a boil. An investipation of the properties
of an acryl-
onltrlle~:rinyl aceta elcqpsl~ ~rt temperatures ranging from 110-25M
and
pressures of 160-IODO kg/cm4 reveAled the oxistence of a minimum in
the similarly---
obtained curves, the temperature of which corresponds to the one at
Which the
!copolymer Aoses its solubility in dimethy1formamide, Orig. art.
hasi 2 charts.
ASSOCIATIOIls none
')Bkug63 00
SUR41TUDs 27Jan62 DATE ACQt 2 ENCL
ISUB COM CH No Ru sov, oo4 0,11MRS 005
Cor4. 2/2

ARZHAKOV, S.A.; RYIDV, Ye.Ye.; SLON1MSKIY,
SIITARMM, B.P.
Role of thermal degradation In the compression
molding of
monolithic solids from powdered polymethyl
methacrylate.
Vysokom. soed. 5 no.10:1513--1519 0 163. WRA 17:1)

ARZHAKOV, S.A.; SLONIKSK37, G.L.; SHTARKW, B.P.;
KARGIN, V.A.
Temperature and pressure dependence of the specific
volume
of polymers. Part 1: Polymethyl methacrylate.
Vysokom. soed.
5 no..12:1854-1860 D 163., (MTRA 17:1)

:ACCESSION NA: A"1780 S/0191/64/owool/0029/0032
AUTHOR:- Arz.4AIQW.,_S.* A*
:TITLEt Effect of strais relaxation an the formation of a Monolithic
solid during I
,pressing of pollmothylostbacrylate-powder
SOURCE: PlastliMsklye mssy*, no. 7, 1964# 29-32
1 TOPIC TAGSt pollymethylostbacry lists, moIJIng, transparency,
powder pressing.
pressed plastics, transparent plastic, stress relaxation, olithic
plastic,
pressing tapperaiture
.4
ABSTRACT: To confl rm previous work In which the production of
transparent plastic
I.specimens was evaluated v1susilly, the authors studied the
transparenci of*3-4xlO- i
!mm samples of pressed polymethyloothecrylate (Mol- we.. 0 300,000
and 500,000) In*
relation to pressing temporatute (0-250C),uslngan IFT-15A photometer.
Transparpnty.."
curves show that products of maximuiv transparency can be obtained at
temperatures
lower than the range of true complete moldebillity. Ilkwever, at
these temperaturest
no strong bond con be obtained bstween the particles., Above the
glass toWgraturell
the product rMlIftl OP44US because of Ahe presence of Internal
stresses. -The
formation of a true monolith'shoWs that a considerable part of the
Internal st'rosses
~jd In the product by the pressure pppjleO to.the powder con be
al.1wlat*d
AN
A.

ACCESSION NRI APW1780
durlngpressilng' -All the foctois'141~~,*
Important role lirl the fo"t,
f ng thm rate Of Stress relaxation play
crYlsteo Orlg* ort6 hall . on 0 i* true Nowl'i th frOR PoWered
polymethyl
flour*s
ASSOCIATiONS rbmw
SUMITTio: 00,
ENCLs 00'
SUB. CODEl OCi- MI,
'NO REVSoVj*',.`O031,~'- arm 060
v
j
b.
q
`A
e A.
ri.., .01
-7-
7
,

Q_Wsf MM i"
ACCESSION NR: AP4043328 B/0191/64/000/008/0051/0054
AUTHOR: Arzbakov, S. A.; Razinskaya, I. N.
TITLE: Dependence of the thermomechanical curves on the conditions
of production of
monolithic samples from powdered polymers
SOURCE: Plasticheskiye massy*, no. 8, 1964, 51-54
TOPIC TAGS: rolyiner, powdered polymer, monolith, suspension
polymerization, thermo-
mechanics, polymethylmethacrylate, polyvinyl chloride, pressed
polymer, polymer
thermomechanical property, pressing, powdered polymer molabig
ABSTRACT: Ilie relationship between the thermomechanical properties
of pressed
polymers and th,,, conditions of production of monolithic pieces
from powdered polymer
material was investigated using polyniethylmethaorylate (mol. wt.
200, 000), obtained by
suspension polyraerization, and polyvinyl chloride (PE-4) (10 min
in diameter, 3 min in
height). The mc1ding process is described; 15 min. was required for
cooling to a tempera-
ture 30-40C lowor than the glass tompuraturo. Thormomechanical
curves wore plotted
with Uio thickneqp gaugo 1ZV-1 at different temperatures and the
same pressure (130 and
190C, ~ 0 kg/cm"), at the same temperature and different pressures
(150C, 2500 and 187
kg/cm~ ) and for the effect of molding conditions cin the
properties, in the region of trans-
Card 1/2

ACCESSION NR: AP4043328
parent and truly monolithic samples. It was found that the
monomer formed during the
molding of powdored polym. ethylmothacrylate decreases*the glass
temperature and the flow
temperature because it plasticizes the polymer. For the correct
determination of the flow
temperature by means of thermomechanical curves, only true
monolithic polymers are
suitable. Since many new polymers are currentlY being produced in
powder form, for
which the transiti;.--n temperatures must be determinod, It Is
very desirable to develop
methods for determining these temperatures on fhe initial polymer
powders without con-
verting them to manoliths. ;-The authors express their gratitude
to Professor G. L.
Slonimskiy for t1he evaluation of this work and the interest
taken in it. Orig. art. has:
6 figures.
ASSOCIATION: None
SUBMITTED: 00
SUB CODE: OC, JUT NO REF SGV: 008
ENCL:00
OTHER: 000
Card 2/2

iACCESSION M AP4017636
S/0190/64/066/002/0253/0257.
'AUTHORSt Ar-!~~ Slonimakiy, Go L.1 Arulint V. I,
.TITLE: The dependenoe of the specific volume of polymers on
temperature and
Pressuroo 2. Polymo--,hylmethaorylate plasticized by dibutirl
phthalate
,SOURCE: V~y*sokomolelculyarny*ye aoyedinehiya, r. 69 no. 2, 1964,
253-257
;TOPIC TAGS: polymeri, polymethylmothaorylate polymerp pla8tioizerf
dibutyl
~phthalate, speoific volume, pressure, critical pressure, heat
expanei0ni vitrifiou-I
i.ion, vitreous state,, high-olsetioity state
!ABST.UCT: In an ear:Lier publication by So A. Arzhakov, Go L.
Slonimekiy, B. P.
;Shtarkman, and V. A. Kargin.(Vy-*sokomolek. soyed., 5, 1854, 1963)
it was shown thatl
'the vitrification tei2perature of pRlymethylmethaorylate (PIMC)
registered a sharp
irise at pressures above 1000 kg/oihl. The present investigation
studied what effect!
the plastification oi! P1121C with 5 and 20/~ of dibutylphthalate
(DBP) would have on
:the specific volume of the polymer, as related to temperature and
pressure. The
'heat expansion of tho PSIC polymer lastioized with 5% DBP," was
recorded at con-
,stant pressures with.1.n a 50-5000 ;~42 range at temperatures up to
350C, as pro-
;sented in Fie. 1 on 1,he Enclosure. As in the case with the
nonplaetioized PWG
Card

'ACCESSION Us AP40117636
po2ymery the V - T cum of Un plasticized PM polymer ohms a sharply
defined
'band between the two stra4ftt-llned sectional sepu%ting the glasm~r
and the hiah
elastic states. With inoreseed, pressureg the T - T curve shifts into
a region of
smaller specific volumes. Similar curves were &Iso obtained with the
P2W polymer
containing 24 DBP. A conparison with corresponding curves of the
nonplasticized
'PWIG polymer revealed a lowering of the pressure above vhich the
glass transition
temperature sets in. This is explained by the fact that the
plasticizer MU
;some of the.free sphoss within the polymer, which "as to be
exhakisted at a pre&-
isure of 2000 kdc=~- Orig,, art*;hasi 6 charts*
I:ASSOCIATIONs. none
SMUEMs 2pov62
ZW AOQs g3l" =MS, 01
SUB CME:. CH SO MW SOTI (M O=t OC"

ACCESSION NR; AP4010760 S/0020/64/154/001/0181/0183
AUTHOR: Arzhal-ov, S. A.; Zaynullin, S. Z.; Shtarkman, B. P.
TITLE: Metlidd of determining polymer transition temperatures by
povder deformation
~SOVRCE: AN SS1.1,R. Dolclady*, v. 154, no. 1, 1964, 181-183
;TOPIC TAGS: polymer, polymer transition, polymer transition
tompera-.
.ture, polymer transition temperature determination, polymer
powder
',deformation
ABSTRACT: A study of polymer trnnsitiott temperatures by powder
deformation is especially ~.mportant because it permits
tracinct,
the powdered system, over a wide temperature range, without
converting
the polymer specimen to a monolithic state. A method is
developed
for determining the polymer transLtion tompera.tures, with the
spe-
cial feature that the thermomechanical curve is plotted bi the
defor-
maLion of the polyiner powder without making it into a block,
The
apparatus 'used is shown in Fig. 1 of tho'Enclosuro. The powder
was
Cord 1/ 3

ACCESSION NR: AP4010760
icompressed at a pressure of 320 kg/cm2 with subsequent reduction
iin load to 40 kg/cm2. The polymer is then heated at a rate of 1C
iper minute with the deformation detormined-over a spoci*fic
tempera-
;ture interval by an indicator with 0.01.-mm graduations. The ad-
ivantage of the method is its high sensitivity in the
dater,mination
!of the glass transition temperatures of crystalline polymers. "The
,authors. thank Academician V. A. K.argin and Profess *or G. L.
Slonimskiy
ifor their interest in this study and for discussion of the
results."
'Orig. art. has: 4 figyres.
!ASSOCIATION: none
iSUBMITTED: 30Ju163 DATE ACQ: 1OFeb64 ENCL: 01
SUB CODE: 00, GO NO REF SOVi 004 OTHER: 000

,CCESSION NRi AP4010760
3/3
C- r 6
ENCLOSURE: 01
Fig. 1. Design illustrating the
principle of the apparatus
1 Die; 2 - plunger; 3 pAnt
of tamporatura.change.

BOKSHTEYN, S.Z.; KISHKIN, S.T.; NIKISHOV, A.S.; POLYAK, E.V.;
SOLOVIEVA, GaG.;
Pr.'Lniza3.i uchastiyes ARZHAXOV,__j.,~q ~ULANGVt A.V.; VERTYUOVAt
L.G.;
KOJUBLEY~; MIRSKIY, PODVOYSXAYA, O.N.1 SAZONOVA, T.N.1
SOWNINAI O.'P.; TITARENKOv I.I.; RINK, L.P.; KOZLOVA, M.N.;
TERMOLOVA, M.I.; MOROZ, L,M.
Ag!Lng of plastically deformed alloys. Metalloved. i term. obr.
met. no.5s4O-44 My 163. 0 (MIRA 1685)
(Heat-resistant alloys-Hardening) (Deformations (Mechanics))

ARKHANGELISK:tY, Pav.P.p agronom-entomolog
Locunts are killed in Kazakhstan. Zaahch. rest. ot vred. i
bol.
2 no.6tl7-20 N-D '57. (MRA 16:1)
(KazakhataA"Lo(iuata--E-.Ktor~~nation)

ARKHANGELISKrr Pe". , entomolog (Alm-Ata)
.9
'Trady" of the Uzakh Scientific Research Institute
for Plant
Protection. Vol. 4. Reviewed by 'P.
Arkhangellskii. Zashch.
raeb. ot vred. i bol. 5 no.10:55,-56 0 160.
(MIRA 16:1)
(Kazakhstan-Plants, Protection of)

--ARZIWV'IFII, N.- G.
"Effect of Antipyrin on the Cardiovascular System." Cand Med Scil,
KharIkov
Medical Inst, Khar`kov, 1953. (KL, No 1, Jan 55)
Survey of Scicntific and Technical Dissertations De-fended at USSR
Higher
Educational Institutiona (12)
SO: Sum. No. 556, ;4 Jun 55

KISLYAKOV, L.D.; BOCHAROV,, V.A.; ANZHANF*OT,
G.I.
Flotation of pyrite with the use of smoke gases.
TSvet. meto
36 )w.4t22-26 Ap '63. (MIRA 164)
(Flotation) (Pyrites)

ARZIIANIM, 14.G.; KRAVETS, N.P.
electrocardiographic changen fol.lowing the Introduction of
oxygen
into the gastrointautinal tract. Mad.parnz.i pnritz.bol. 33
no.4j
425-430 JI-Ag 164. (MIRA 18: 3)
1. Kafedra obshchey terapii Stamislavskogo meditsinskogo
institutA.

ARZIUNIKOV, N.S.
K teorii pod"emnoi. sily i lobovogo soprotivleniia prof.
Vitoshinskogo.
Foskvaj 1929, 13 11, (TSAGI. Trudyj no. h8)
Sumary in English.,
Title tr.: Prof. Witosz.Nmski's theory of lift force and drag,
Cf. Witoszynski, Czeslaw; La mecanique des profils dlaviation.
QA!?ll,m65 no-48
SO: Aeronautical Eciences and Aviation in the Soviet Union,
Library of Congress,,
1955

XZHA V /A-ov~ A? 15
CHAPLYGD) SYRMI ALEYSPEVICH, and N. S. ARMVIIKP~)
K voprosii o deformatsii tri-,by, ogranilchennoi (Womia
ekstsentricheskimi
tsi.lindrami '. szhatoi postoiannym davlenieT-J. ('P"IAC.I. Trudy,
1933,
110. 123, p. :L3-25, dii!-rs.)
Sumary in Enrlish.
Title tr.: Deformation of a tube bounded by two eccentric cylJMders
and
svb'iectp~ to a constant nressure.
QA911.M65 no. 123
SO: Aeronavitical Sciences and Aviation in the Soviet Union, Library
of
Conrress, 1955.

PHASE, I THEASURE ISLAND BIBLIOGRAPHICAL REPORT AID 203 1
BOOK Call No.: AF603637
Author: ARZHAN 'IKOV N. S., and MALITSEV, V. N.
Full Tit16---A-V05~Afm~6
Transliterated Title: Aerodinamika
Publishing Data
Originating Agency: None
Publishing House: State Publishing House of the Defense Industry
(Oborongizj
Date: 1952 No. pp.: 480 No. of copies: Not; given
Editorial 33taff
Editor: None Tech. Ed.: None
Editor-ln-Chlef: None Appraisers: Professors
Kamenkov, G. V., Martynov,
A. K., Nuzhin, S. G.;
Dotsents Putyata, V. I.,
Lebedev, A. A.
Others: Aspirants of the Moskva Aviation Institute Kotlyar, Ya. M.,
Sad~~kova, G. S., and Orlov, R. A~
Text Data
Coverage: This is a textbook on theoretical aerodynamics. The first
1/12

I tin m I kn AID 2031 - I
two-thirds of the volume describes the bagic ideaL nd con-
ceptions of the hydro- and aerodynamics of incompressible
flulds, the second part Is dedicated to the aerodynamics of
hIgher velocities (
gasodyvamics). Diagrams, graphs, photos,
etc .
rhAg Is a well-compiled and up-to-date textbook on aerodyna-
ni(-~i. It is most comparable to L., Prandtl's Essentials of
'.FlUi Dynamics, 1952 or to M. Rauticher's Intr tion to
Bynamics, 1953, though *it is shorter Fh_aneit=
Aeronau Ml~
TABLE OF CONTENTS PAGE
Ch. I USSR - The Birthplace of Aerodynamics 5 - 17
Development of hydro-and aerodynamics in the
XVIITth and XTXth centuries in Russia;
Zhukovskiy., N. Ye., and Chaplygin, S. A.,
founders of contemporary aerodynamics; Leading
Rolf of Soviet scientists in the development of
aerodynamics.
Ch, II BaBic Ccneeptions of Hydro.- and Aerodynamics 18 -- 25
Conception of fluid mass and weight density;
ClassMcation of fluids; Conception of hydro-
2/12

Aerodinamika
AIP 203
pAvr~
dynamic pressure in a given point of a fluid;
Classtfication of forces acting in a fluid;
Indep,endence of the hydrodynamic pressure-in
a perfect fluid from direction.
Ch. III Kinematics of Fluids 26 71
Euler's method; Lagrange's method; Classifica-
tion of fluid motion; Flow line; Equation of
continuity; Circulatory flow; Movement of a
fluid particle; Potential movement of a fluid;
Equation of continuity for a protential move-
ment of a fluid-in rectangular coordinates and
in polar coordinates; Velocity circulation in
a potential flow; Fundtion of a flow; Method
of superposing-potential flows; Rectilinear
uniform flow; Flow inside a straight angle;
Flow and source; Dipole; Vortex; Flow around
a circular cylinder without circulation, and
with circulation.
Ch. IV Principles of H7drodynamica of a Perfect Fluid 72 90
3/12

AerodinAmika
A IJ 203 -, I
Differential equation of movement of a perfect
fluid according to Rulerp and according to
Gromeko; Initial and boundary conditions; In-
tegrals of differential equations of movement;
Limits of application of Bernoulli's equation
to air; Distribution of pressure, outside and'
inside a two-dimensional vortex.
Ch. V Principles of Vortex Theory 91 112
Conception of a vortex line; Vortex tube;
Stokes' theorem; Thomson's theorem on
uniformity of circulation; Helmholtz's
theorem on vortices; mot-Savart's,formula
on vortex effect; Problem of determination
of vortex effect in a general case;.Buler
-D'Alembert's paradox; Zhukovskits theorem.
Ch. VI Application of the Theory of Complex Varia)ile
Function to the Study of Two Dimentional Parallel
Flow or a Perfect Fluid . 113 - 136
Complex potential; Complex velocity; Examples
of simpler flows; Movement of a vortex pair;
4/12

AerodAnamilka
20-~
FAGE
Vorl.c-x filament; Conception of ~rortex trailt
Flor around a circular cylinder; Deduction
of ooi!iplex velocity; Zhukovskly-Chaplygin
theore-m on resultant force of pressurez-
Cli3plyginls theorem on the moment of t1w
reaultant force of pressure.
Ch. VIT Theory of' a Wing in a Two Dimensional Parallel
F I o-,- -137 181
'.'oricept of conforml representation,- Examples
2T isimpler conformal representatione; Trans-
forrwil.lon of inverslon.,r ZhukovskWs trans-
Toriratlon,, Zhukovskiy-Chaplygin Profiles'-.
Graphical method of desIgning Zhukovskiy-
i1whaplygin profiles; Determination of the value
of the lifting force of the theoretical.
4,hakovskiy-ChaplygAn profile; Theoretical pro-
1.,llei3; Calculation of the forc2 And of i-J.,(:
raornent. for a profile of an arbitrary for~n,
Theor-y of a thin alrfoil~ Formation ot it -pL)-
tential flow around the airfoil of a wing of an
r1rhitz-ary form (S~ G. Nuzhinrs method),
5/12

Aerodinamika
Alj~: ")O*.j - I
PAU,
Ch.V111 Theory of A "Slipstream Drag and of a Vortez
Draf,
cof a slipstream flow around a body-,
Tlm- of a flow arotind a f lat pirtio
with !01 ipatream formanon; Concept of
vorte, reststance.
Ch. IX Pr1ricipleii of the Theory Of Vlacous Fluld
movement 1,YT 232
Differential equations of viscous incom-
pk,o1-.1,:j1b1e fluld movernent.~ Conception of
~4 impil-itude criteria ; Laminar f Low of
61 vlvcous fluid in a circulay-
plpe,, ,"oncept of turbulent flowJ, Turbulent
fiovi In itralght and curved pipes-
Ch. X 13 o u ri (I ~,, r 273
y Ut y e r
of the boundary layer; Differential
coo-ition of the boundary layer; Integral
c6nvo-tiitlon of the boundary layer, Calclila-
tlort (if the laminar boundary layer for a
I'lat plate; Calculation of' a turbolent
611-,~

Aerodinamika AID 203 1
PAR
boundary layer fox, a flat plated Calculation
of a mixed boundary layer for a flat plate;
Boundary layer on a curved surface; Calcula-
tion of a laminar boundary layer for a curved'
31117face (L. G. Loytayan(skiy's method).
Ch. X1 Theory of Finite Span Wings 2T9 310
Hydrodynamic models of a finite span wing;
Conception of the downwaBh and of the Induced
drag force for a finite span wing; Induced
velocity and the downwaBh of the stream; Forces
acting on a wing; Induced drag; Principal
Integral-differential equation of a finite span
wing; Approximate method of calculation of the
distribution of the circulation along the wing's
span; Determination of the lifting force and of
-the induced drag of the wing; Formulae for
t,.hecking wings not rounded off from one elonga-
.,ion to another; Most convenient form in a
plane projection of a finite span wing; Solving
of the integral-differential equation of a wing
by S. G. Nuzhin's method,
7/12

Aerodinamika AL
203 - I

PAGE
Ch. XII BaEdc Information on
Thermodynamics
'11-1 - 318
Equation of the state of the gas;
First law

of thermodynamics; Thermal capacity; Heat

content;
Second law of thermodynamics; Entropy.

Ch.XIII System of
Basic Differential Equations in Gas

Dyriamics
319 - 32-D
The
setting of the problem and the basic

equations of gas
dynamics; Equations of energy,.

Ch. XIV Uniform !so-entropie
Gas Flow
324 - 338
Principal correlation for uniform. iso-,

entropic gas flow; Connection between the

velocity of the gas
flow and the form of

it5 stream.

Ch. .-N Theory of the Norml
Shock Wave
339 - 354
Principal correlations of the normal
shook

1weve; Comparison of the condensation in

noriml
shock-wave with iso-entropic conden-

i3atlon.; Velocity of
the pressure wave propa--

gatlon~ Sound wave; Pressure In the
critical

point behind the normal shook wave,

4112

Aerodinamika An 203 - I
rAGE
Ch. XVI Two-dimensional. Supersonic Gas Flows 355 382
Criteria of potentiality for a two-
dimensional iso-entropic gas flow; Basic
differential equation for a two-dimensional
potential gas flow; Characteristics in the
plane of the gas flow; Characteristics in
the plane of the velocity hodograph; Deter-
mination of the orientation-of characteristics
in the~'plane of the gas flow and in the plane
of the velocity hodograph, according to a
given vector of velocity and with help of an
iso-entropic ellipse; Determination of the
field of velocities in a two-dimensional
supersonio potential gas flow by the method
of characteristics; Supersonic'flow around
a convex obtuse angle.
Ch. XVII Theory of an Oblique Shook Wave 383 392
Conception of an oblique shook wave;
Determination of gas parameters behind an
oblique shook wave; Connection between the
9/12

Aerodinamika
deflection angle of a supersonic flow and
the position of the front of an oblique
AID -203 1
PAGE
shook wave; Polaris of shock.
Ch.XVIII Principles of the Theory of the Profile and of
the Wing in a Subsonic Plow 393 435
Concept of the critical number Mkr;
Approximate wing profile theory up to the
critical ;e ion (Method of reduction to the
linear fo m~ ; Equation of Chaplygin for the
study of gas flows of higher oubsonic
velocities; Method of Khristianovich, S. A.;
The approximative theory of Burago, 0. F. on
the subsonic flow around arbitrary wingpro-
files; Influence of compressibility on the
magnitude of the induced velocity of the wing;
Finite span wing in a flow of compressible
fluid at subsonic velocities; Flow around an
airfoil past the critical region; Calculation
of the wave resistance by the Diethod of
3urago, G. F.; Aerodynamic characteristics of
a profile in a critical region.
10/12

Aerodinamika
AID 203 - I
PAGE
Ch. xjX Principles of Profile and Wing Theory in

Supersonic Oas Flow
436 469
Concept of a linearized supersonic
flow

of rarification and compression of gas

along a firm
boundary; Linearized theory

of a supersonic flow around a
flat plate;

Linearized theory of a supersonic flow

around a
thin profile; M,)re precise theories

of a profile'-ih
supersonic flow*- Precise

solution of a problem concerning
the flow at

supersonic speed around a profile composed

of
straight sectors; Aerodynamic forces

acting on a flat plate
of infinite length

sliding in a supersonic flow; Statement

of
the problem of a finite span wing in a

supersonic flow;
Rhomboidal flat wing.

Literature
470 473
Furpose: A,,,cepted by
the Ministry of Higher Education of
the USSR
aa a textbook for
aviation universities. It may
be
uiieful also to engineering
technical workers of
aviation
11/12

Aerodinamika AID 293-- -
plants and design bureaus.
Facilities: Large number of Russian scientists *mentioned in
the text
No. of Russian and Slavic References: 17 prior to 1939, and 57
after
this date
Available: A.I.D., Library t)f Congress.
12/12

Call Nr: AF 1073605
.AUTHOR: Arzhanikov, N. S., and Malltsev, V. N.
TITLE: Aerodynamics (AerodinaMika)
PUB. DATA: Cibor'ongiz,'Moscow, 1956.. Second =tion..:484 pages.,
8,500 copies
ORIG. AGENCY: None
EDITOR: Kotlyar, Ya.M., Candidate of Technical Sciences;
Managing Editort Sokolovp A, I., Engincerl Editor of tho
lublishing House: Petrova,.I. A.; Tech. Ed.: Gladkikh, X.N.
Reviewers: Burago, G. F., Doctor of Technical Sciences,
Frofes3or,, Votyakov,, V. D., Candidate of Technical
Sciences, Docent, and Shumyatskiy, B.Ya., Candidate of
Technical Sciences.
PURPOSE: The book is approved by the Ministry of Higher Education
as a textbook for students of advanced courses at aero-
nautical engineering schools and can also be used by
aircraft engineers and researchers. It is based on
courses of lectures oh Aero- and Gas Dynamics given at
the Aircraft Construction Department of the Moscow
Card 1/4 Institute of Aviation.

.Aerodynamics (cont.) Call Nr: Af 1073605
:COVERAGE: Several sections (IV.. 5; V.. 6 and l1,, xii., 6., and
XIII.'..-4)
were not contained in the first edition.
Chapter IV: Principles of Hydrodynamics of a Perfect Fluid
Section 5: Momentum equation for steady motion of a perfect fluid
Chapter V: Principles of Vortex Theory
Section 6: Pressure distribution inside and outside a plane vortex
Proof of N.Ye. Zhukovskiy's theorem for an arbitrary
Section 11.
two-dimensional contour
Chapter XII: Gas Dynamics
-Section 6: Speed of sound
Chapter XIII; System of Basic Differential Equations in Gas
Dynamics
Section 3: Umits of the application to air of Bernoulli's equa-
tion for incompressible fluids.
Card 2/4

AerodynamicB (Cont.)
Call Nr: AF 107,,;605
There are indications of some efficient methods.for the solu-
tion-oj",particular problems developed by USSR researchers.
These,are: a) The method of S. G. Nuzhin for "construction of
airfoil"'
the poi,,ential'flow about an arbitrary-
Ichapter VII,
section 10.- For the same purpose, the methods of
Th. Thoodorsen, Lighthill, and Goldstein are widely used in
the U.S.A; b) The method of L. 0. Loytsyanskiy for "the de-
terminUtion' (calculation') of the laminar boundary layer for
curved surfaces", chapter X., section 8. This method is recom-
mended by the authors of this book as more accurate and easier
for computing purposes than that of Kaman-Pohlhausen. It is
also applicable to the symmetrical flow about bodies of
revolution (fuselage, etc); c) The,method of S. Q.- Nuzhin for
nablution of the integro-differential equation of an airfoil
of finite aspeet ratio". chapter XI, section 9; d) The method
of S. C1. Khristianovich for problems of airfoils and wings in
Card 3/4 subsonic flo*s, chapter XVIII, section 4; h) The
approximate

Aerodynamics (cont.)
Call Nr: AF 1073605
theory of the subsonic flow around arbitrary wing profiles by
14 F. Burago. This book contains very few numerical examples
but there I's a considerable number of analytical (algebraic)
problems with q6lutions clarifying pertinent cases. The
number of references, all USSR, has been increased to 85.
AVAILABLE: Library of Congress
Card 4/4

ARZHANIKOV, N. S. Prof.
"Utilize the Scientific, Cadres of Higher Schools More
Fxtensively,n Vest.
Vysshey Shkolys No.9j, 1955.
Main
Head,/Administrztion of Polytechnic and Machine Building VuZes,
Ministry of Higher
ation USSR.
Translation W-31694, 16 YAr 56

IJMEIW, A.A.; TIMNIN, A N.; AltZH&NIKOV, I.S.;
BOGORODITSKIT, N.P.;
I)MDLIN, N.P.; OD;NTiOv"%V.,r,-,*ftbtb#. S.Ta.
Profismeor B.P. Kozyrev. Blaktrichostvo no.1:94 Ja
'56. (VLRk 9:3)
(lozyrev, Boris Pavlovich)

SUBJECTs USSR/Lenin Awards 25-5-1/35
AUTHOR: Arshanikox.-I.P.-. Scientific Secretary to the Lenin Awards
Coanittes for Science and Engineering
TITLEs Lenin Awards (L*ninskiyo Proaii)
PERIODICALs 1auka I Zhisn' - May 1957, No 5, pp I - 2 (USSR)
ABSTRACTt 'rho first Lenin awards were distributed in 1925, when
in-
itiated by the Comunist Party and the Soviet government to
ioncourage scientific work in the fields of science, engineer-
Ing, agriculture, medicine, and social sciences. Also in 1957
thost awards have beendistributed after very careful examiD,-
ation of the scientific material to stross their importance
:ror the entire nation. So# for instance, the scientists who
built the first atomic electric power plant for industrial
purposes in the world got the Lenin award. Aoademioian N.X..
3avoymkiy earned his award for discovering and studying the
phenomena of paramagnetic resonance. Soviet biologist B.A.
Dog*11 got this prize for his research work on protistolegy~.
A whole group of geologists was distinguished for disooviring
diamond deposits In West Yakutiya and another group of~lgoo-
Card 1/2 logisto got their award for finding the largest iron ore
doo

TITLE: Lenin Awards (Leninskiye Premii) ;25-5-1/35
posit,in the USSR. Academician A.#. Tupolev eaxaed h1s:priss
for construoting the passenger turbo-jet plane "TU-104". An-
other prize was awarded a group of constructors who Introduced
the full autonatization of industrial proossees for the mass
produotion of bearings. The Lenin prizes have proved to be
,Y*ry inspiring to the workers of Soviet science and engineer-
Ing.
ASSOCIATION:
PRESENTED M
SUBMITTEDt
AVAILABLE:
Card 2/2
/V Y/
k1
-5-1F ek x,
< Ta,
J, /7 A-X)

KWNOV, NikiDW Fedorovich; ires., prof.. reteenze'nt;
SHDWMaY,
B.Te., kau4, takhn. naut~ i;4~'tOsiwIfit'VxUZwSOTO SOIOO
kand. takhn.
muk~ reteensont; EUSILIN110t, S.M., lush., red.;
TUBTAIMUU, 7.G.,
Izd-vu red,; PUKHL3XOVA, N.A,I, teltn. red,
(Aerodimmic's of-rotating bodies) A~rodima-ika te'l
vrashchenlia'
Wskm~ Goo; izd-vo obor. promWehl,, 1958, 560 pe" WRA na;)

AUTHOR: Arzhanikov, N.S., Professor 3-58-4-27/34
TITLEt Th,9 System of Engineering and Technical Education in
England
(Slatema inzhenerno-tokhnicheakogo obrazovaniya v Anglii)
PERIODICALt Veiitnik Vyeshey Shkoly, 1958, # 4# Pp 75 - 80
(USSR)
ABSTRAM The author presenta a detailod report on higher
technical
editoation in England which he visited with a delegation of
workers of Soviet special institutes.
AVAILABLE# Library of Congress
Card 1/1

D237/D304
AUTHOR: Arzhanikov, N. S.
TITLE: S. A. Chaplygin (on his 90th birthday)
PERIODICAL: Referativnyy zhurnal, Mekhanikat no. 1, 1962,
4, abstract 1A16 (V ab. Vopr. istorii yeste-
stvozn. i tekhn. no. 10. M., AN SSSR, 1960,
42-48)
TEXT: A short bibliographical note is given together with
the more important results of S. A. Chaplygin's work in analyti-
cal mechanicaq rigid body dynamics, ballistics, applied mathe-
matics, hydrodynamics, and, in particular, problems in
aerodyna- V/
mics and gas dynamics. The main achievements of Soviet scien-
tists, who developed and continued S. A. Chaplygin's researches
on various separate problems, are also discussed. CAbstracter's
note: Complete translation.~7
3/124/62/000/001/001/046
Card 1/1

ARZHANIKO'r N.S.; SADEXOVAj G.S.; DUBASOVp V.T.p
reteenzent;
KA . rotsenzent; PRATUSEVICH, G.M.,, red.;
. CAVRILOVA, TA, 'red.
[Supersonic flow about bodies of revolution]
Obtekanis tal
i-rashcheniia overkhzvukovym potokom. Moskva, Moak,
avitatai-
cr~~ in-t im. Sergo Ordhonikidze, lcXi2,) 65 p.
(MIRA 1614)
(Aerodynamics, Supersoid I

ARZHANIKff,_ N~._-prof 0
Pride of our science and technology, NTO
1. Uchenyy sakretarl Komiteta po Leninakim
i -takhniki pri Sovete Ministrov ESSR,
no.6:21-24 JS '63.
(MM 16:9)
promiyam v oblasti nauki

KRASNOV, Nikolay
Fedor-ovich;,,ARZI"111;OV,,~..,).~ prof.,
retsen.ent;
EOTLYAR, Ya.M., dot 0 - -
[Aerodynamics of bodies of revolution]
Aerodinamika tel
vrasbehaniia. Izd.2., 1;erer. i dop, Ylookva,
Mashinostro-
enie, 1964. 572 p. (MIRA 17:10)

_AC____ --_~6- M-o- n--og r---a-p-
C NR.AM610_055 4
Arz.hanikov., N.Lkolay Sergeyevich; Sadekova, Galina Sadekovna
High speed ae:1,odynamics (Aerodinamika bol'shikh skorostey)
Moscow,
Izd-vo "Vysahaya shkola".. 1965. 556 pillus,., biblio, Errata Blip
inserted. E100o copies printed. A textbook for students of higher
aviation schools and faculties.
TOPIC TAGS: aerodynamics, gas dynainics, hyp'ersonic
aerodynamics,,
supersonic aerodynamics, magnetogaadynamies, boundary layer,
aerodynamic heating, rarefied gasdynamics, couette flow,, free
molecular flow, aerodynamic lift, aerodynamic drag
PURPOSE AHD C(WERAG13: This book is intended for students of aero-
nautical enEinecring and similar specialties. It can also be used
au a textbook by scientific personnel of design bureaus and
researoh'
institutes. It is based on a lecture course on theoretical and
applied gas dynamics given at the Moscow Aviation Institute Im,
Sergo Ordzhonikidze and provides a full-scale trentise of the
AmdamentalEt of high-speed acrodynamics. It is divided in 14
Chapters, 9ho'-first six chapters are concerned with theoretical
Card 1/4

ACC NRdV'1OQU55u4
aspects of oubsonic and supersonic gas dynamics, and shock wave
theory. The next two chapters deal with the wing profile theory
in subsonic and supersonic flows and contain descriptions of
Chaplygin's and Khristianovichlo methods for Investigating gas
flows at high subsonic speeds. Chapter 9 is concerned with the
theory of finite span wings in supersonic flows and gives methods
for determining the aerodynamic properties of rectangular and
delta
wings. Cha~pter ten deals with the theory of supersonic flows over
bodies of r-~volution at an angle of attack and with applications
of
the method of characteristics to determining velocity fields.
Chapter ele,ten is concerned with the principles of hypersonic
aerodynamic,,3, its peculiarities, and the application of
hypersonic
similarity law. Chapter 12 deals with the problems of the boundary
layer and aerodynamic heating at high speeds, Chapter thirteen
Is concerned with aerodynamics of rarefied gases, slip flow,
and free-mo:lecular flow. Chapter fourteen deals with the
principles
of magneto-gae dynamics, studies of charged particles motion and
Couette flow, The authors express their thanks to reviewers:
Professor N,,F,Krasnovp Associate Profesoors V,NsKoahevoy and A.
N.
Danilov, aloo to Professor G, Fe Burago for his valuable remarks
and advice.

4C -NRIJU-10005504
TABLE OF COMENTS (abrideed]:
Foreword -- 5,
Introduction -- 7
Ch.l. Basic data from gaadynamics and thermodynamics -- 9
Ch.-11. Fundamental differential equations of ioentropio gau
flow 34
Ch,III, One-dimensional iBentropic gas flows 52
Ch.IV. Theory of straight shock waves -- 69~
Ch.V, Theory of oblique shock waves -- 8g
Ch.V1. Two-dimensional supersonic gas flows 102
Ch.VII. Principles of wing theory at subsonic sPdeda 133
Ch,V111. Principles of wing theory at supersonic speeds -- 176

-A-C-C--N--k';-jI~j-6 bb-~5~ 4
- Ch,IX, Theory of finite span wings in supersonic flows 2o6
CII.X. Theory of supersonic flows over bodies of revolution 281
Ch.XI. Principles of hypersonic aerodynamics -- 348
Ch,XII. The boundary layer and aerodynamic heating at-high
Bpeeda.-
410
Ch.XIII. Certain problems of rarefied gas aerodynamics 493:
Ch.XIV, Principles of magnetogaodyncimics -- 516
Bibliography 553
SUB CODE: 20/ SUM DATE: 02Julo'V ORIG REF: 022/ OTIM PM,:CO07
Card 4AL

BOCHAROV, V.A.; KISLYAKOV, L.D.; ARZHANNIKOVp G.I.
Ways of improving the quality of concentrates during the
dressing
o:~ Ural copper-zinc ores. TSvet. met. 36 no.8:12-16 A
163.
~HIRA 16:9)
(Ural Mountains--Nonferrous metals)
(Ore dressing--Quality control)

KISLYAKOV, L.D.; BOCHAROV, V.A.; ARMAIMMV, G.I.
- ,
T
jilatation practices of Ural mountain pyri.tos and
wiys of
I.mproving the qualitative indices of ore
dressing. TSvet. met.
)7 no.6:11-14 Je 16/. (141RA 17s9)

I
CURSKIYp P.A.; MERRO, ye.M.; KHUTOIffJWSKI'Y,
N.M.; ANISMV, N.M.;
ARZRIURMOV, S.M. KOREIMSKIYII M,V,j inzh..,
retsenzent;
STEV~K6~ Ye.G., kand. tekhn. nauk.. retsenzent;
SOBAKIN,
V.V.y inzh., red.; VASILIYEVA, N.N.,, tekhn. red.
(Experience in the organization of railroad
laboratory for
the inspection and maintenance Of measuring
equipmentlopyt
organizataii-dorozhnoi kontroll:no-izmaritelinoi
laboratorii.
Moskvap Transzheldorizdat, 1962. 167 p. (MIRA
16:1)
(Railroads-Equipment mad supplies)
(Moscow-Testing laboratories)

ARZIIAI;NlXCV. Ye.P.1 WN"p A.A.
--, ,
Optimal characteristics of low-frequency filters.
hadiotekh-
rdka 20 no.10%21-30 0 165. (."Ir" le,11)
1. DayBtvitell We ohleny Nituohno-tvkhnicheakogo
obahchostva
rddiotakhniki I elektroavyauie

:: olme 0*0*000*000*
0660646660609 4, 0 e
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100
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MOO
roe

GORDOV, A. N. ; ARZHASOV, DIUOVI U.V.
T!L-LA!j
Now determination of the solidification
temperature of pure
gold* DDkl.AN SSSR 133 no.4:611-812 Ag '60.
(MIRA 13t7)
1. Vsesoyu&Wy nuacbno-issledovatellskly institut
metrologii.
imeni D,I,Mendeloyeva. Predstavleno akademikom
A.A.Lebedevym.
(Gold)

S/08 61/000/010/001/029
BI 17XB207 -
AUTHORSs Arzhanov, A. S., Gordov, A. N., Diykov, U. V.
TITLE: New methods of determin!,ng the solidifioation
temperature of
pure gold
FERIODNAL: Referativnyy zhurnal. 1(himiyat no. 109 1961, 50,
abstract
106342 (10B342). ("Tr. in-tov Kom-ta standartovImer i
izmerit. priborov pri Sov. Min. SSSR", no. 49 (109), 1960,
5-12)
TEXT: This paper presents results obtained when determining
the thermo-
dynamic solLdification temperature of pure gold by means of a
nitrogen-gas
thermometer of constant volume. Test results of the newly
constructed gas
thermometer and the pressure coefficient of the operation gas
are given.
The solidiqM,,ation temperature of gold was found to be
1064-50 + 0.20 C.
Abstracte:~'s note: Complete translation.]
Card 1/1

ARZhANOV, D.
Sbornik upr.Rzhneniy po kursu "Nalogi I
(Collection 01' Exercises For The Course
From Collective Farms And Individuals".
Moskva, Gosfinizdat, 1954.
N15
771.211
Sbory S Kolkhozov I Naseleniyatt -A7
On "Taxes And Duties Collected
By) D. Arzhanov 1 0. Tsalkin.
106 p. tzbles.

ARZHANOV, Felike Grigorlyevich; MIKMEV, N.L.,
red.; DUIASOVA,
tod.
[Completing injection wells and increasing their
intake
capacity; practices of the Oil Yield
Administration of the
Pervomayskiy Petroleum Trust] Osvoenie i
uvelichenie prie-
mistosti nagnotatellrorkh skvazhin; iz opyta
neftepror~yslo-
vogo upravleniia "Pervomainoft'.11 Kuibyshev,
Kuibysbevskoe
knizhnoe izd-vo, 1963. 36 p. (MIRA 17:1)

61384
e.
S/020/60/132/06/01/068
C 111/C 222
AUTHOR: Arzh2,~~~ &
TITLE: Nonlinear Riemannian Type Boundary Va,lue Problem
PERIODICAL: Doklady Akademii nauk SSSR, 1960, Vol. 132, No. 6,
pp.1227-1230
TEXT: D+ Let,the simple smooth closed curve L divide the z-plane
into the do-
mains and D- (external domain). The author seeks the functions ~
+(z) and
-W analytic in D+ and Di respectively, which on L satisfy the
relation
M (t)] n - G(t) P _(t) + 9(t)
where G(t) and g(t) on L satisfy the Hdlder condition, G(t) ~ 0 , n
>,,2 and
integral. By the substitution
(2) +(z) n -(z) _(Z)
"Ic,
the nonlinos.r problem is reduced to the linear Riemannian boundary
value
proble in order that 1-f+(Z) (z) O-W in a
Card 12*3 1

81364
Nonlinear Riemannian Type Boundary Value 3/020/60/132/06/01/068
Problem C111/C222
solution of (1) it is necessary and sufficient that has no rami-
z)
(z
fication points in D . It is shown that the problem is always
solvable for
)C W ind G(t)?,O namely it is
r +Z)
(5) +(z) _ e n -(z) - er
0 )~-Pa-ew+ P+(z), ~ z Pm(z)+ F-(z)]
where (z) - 1 In [t-MG(t)l dt I F(.) - I g(t) e- r+(t)
21r i t 2#C i t - z
L L
PX (Z) coz he + ciz at -1+ + ok f ci complex constants. For 1
(1) is not solvable with g(t) z 0 ; if g(t) ~*O , then the
problem is
solvable only if 1) ~ g(t) 0- r +(t)tM-1 dt~O,mal, 1 and
L
2) ~9/-j;Fz) contains no ramification points in D+ ; then the
solution is
Card 2/3 ->~

8138h
Nonlinear Riemannian Type Boundary Value S/020/60/132/06/01/068
Problem ,- C111/C222
given by (5) with Pe(z) a 0. Finally it is inveatigated how
far the coeffi-
cients a of P
i ,,(z) are arbitrary. It is stated that the number of
additional
conditions to which the c i can be submitted, depend in
essential on these
conditions theriselves. The author investigaten the question
how many con-
ditions of t)ie.kind:()+ (Zi) - ai b can be given. There are
5 theorems. 1,?he il'uthor mentions V.K. Natalevich and P.V.
Solov'yev. He
thanks F.D. Gakhov for the leading of the work. There are 5
Soviet re-
ferences.
ASSOCIAITION.-; Rontovskiy-na-Donu gosudaretvennyy universitet
(Rostov-na-
Donu, State University)
PRESENTEDt February 24Y 19600 by P.Ta. Kochina, Academician
SUBKITTEDt February 15t 1960
Card 3/3

5411 ;'9'~61/002/004/001/007
B11 2/B108
AUITOR: Arzhanov, G. V.
TITLE: Nonlinear boundary value problem of the Riemannian type
PERIODIdALt Sibirskiy matematichaskiy zhurnal, v. 2, no- 49
1961* 481 504
TEXTs The author studies the following boundary value problem:
In the *A=
P.
of complex numbers a smooth olosed ourve L separates an internal
domain D+
from an external domain D". The functions 0+(z) and 0-(z) which
are
analytic in D+ and D-, respeotiVely, and which, on L, satisfy
the relation
I ~(t) n , G(t) 0-(t) + g(t) (n beinj: an integer > 1) are
required. G(t)
a! g(t~ are given functions which satisfy H61der's condition. GM
must
not vanish. The solvabilit of this problem mainly depends on the
indox of G_
ind G(t) - (S) ~d(G(t)~* Among other things the author
demonstrates
that the homogeneous problem (g(t) - 0) can be solved only for X
> 0. if-'~".
;e >0, the inhomogeneoue problem can be solved for any free term
g. If
X 4 09 the problem cannot be solved. Professor F. D. Gakhov is
thanked for
help. There are 6 Soviet references.
CarA:J~

- ARZHANOV, G.V.-
3olvability of one type of nonlinear boundary value
problems.
:Dokl. AN SSSR 139 no.2:267-270 Jl 161. (MIRA 14:7)
14 Rostovskiy-na-Donu gosudarstvennyy univorsitet.
Prodstavleno
idmdemikom P~Ya. Kochinoy.
(lbundary value problems) (Oporatore (Mathematics))

SU!"I
ACC NR, x.,030,80 SWICCI., CODL; Uft/0000/66/OO0/"/O0)4/0*'
f
AUTHOR: An-banoUJA-9-s.; Deregovkin, A. V.; Dryanov, Is I.;
Dqytuiov,_~, V.;
Zal~ogu,rvj S. N.; Kamontshchiko , Yu. V.; Kovnlov, V. V.;
Krasovskiy, A. S.;
)wznetsov -'S.' V. LiCi- "'*-A'.*' 'Y
-0-Y)". N.; Nikitinj._4~yp; Nistratov,_~s_V.; Poruchi~ov a
Potkin, V. Yes; Teretlyey,_.Kt~.; Fedorov,.Ye. A.; Khlebnikov, G.
F.;
Y
ORC~. none
TITLE: Results of clinical and physiological investigations of
the crew of the
first multiman Voskhod 'ppacecraft Raper r9sented the Conference
on Problems of
Snace Medicine hold in Moscow from 24 to ~7 May 1969) .
SOURCE: Konferentsiya*~o problemam kosmicheskoy meditsiny, 1966.
Problemy
kosmicheskoy meditsiny. (Problems of space zwdicine); matorialy
konferent0iij
Moscow, 1966, 34--36 F
TOPIC TAGS: space medicine', space physiology, weightlessness,
bodily fatigue,
stress reaction, combined stress, cardiovascular system, central
nervous system,,
manned spaceflight/Voskhod-1 S/ ,/
ABSTRACT: The inclusion of a physician in the crew of the
Vookhod-1 made ~t pos~-
sible to increase medical investi'gation's of the crew
mer0beiiii-during'
,flight and to compare them with results of preflight and
postflight exami-
.nations. The scope of the physiological examinations was
selected in
l'order to obtain a more complete evaluation of the functional
condition of
'the cardiovascular and central nervouq.systems, and the function
of
&rd 1A

L 08269-
ACI~ NRs
external respiration of 'the cosm'onauts. Physical exercises
and ortho-
static tests were included to detect earlier signs of
physiologic.-II ahifts.
Examinations were carried out before and after training in the
ship,
-where certain conditions of night were simitlated, and also
two weeks
.before flight. Postflight examination was begun fifteen
minutes after
-landing and was continued for the first four days after the
flight and alaD
'two weeks later.
After landing. the cosmonauts were actfve, looked somewhat
excited.;!
and complained of general fatigue. They were found to have
hyperemia
of the mucosa of the upper respiratory tract and
conjunctivitis.
Xomar.ovI a weight dropped by 2. 616, FeoktistovI s weight
dropped by
.414, and Yegorov" s by 3. 976, Weight loss was determined by
Zhdanov to
be -due to waier and fat loss. Neurological examination
revealed a light
,swaying in the Romberg position, a tremor of the fingers, and
increased
perspiration. In addition, Yegorov showed a contraction of the
retinal
arteries. Disruption of vision and vestibulav difficulties
were not noted.
,Changes in EEG indicated an increase in. inhibitory
proce'sses in the
~,pprtcx of.the brain. Adiminution in work Capacity was
established-by

J_'ACC NR, 41,60364B6
psychological e)q)erIments (Incrense In the! number of mistakes,
Increase*
in latent periods).
Indices of cardiovascular activity during rest did not exceed wide
norms. However, an increase in pulse frequency was noted (Komarov
up to 96, Feokl:istov up to 100, and Yegorov up to 94 beats/min), as
well as moderate drop in arterial pulse pressure at the expense of
an
.increase in diastolic pressure. All three cosmonauts, when
subjected
to exercise, showed a significaht Increase ih the pulse rate and
inertia I
in the stroke volume. Feoktistov and Yegorov showed a significant
diminution in the heart stroke volume and minute circulation of the
blood
during the passive orthostatic test. This could indicAe a
discuption of
the venous inflow to the heart.
Postflight:alood examinations indicated neutrophilic leukocytosis
-and eosinopenia. Urine was found to contain significant quantities
of
salts, chiefly uratcs, single erythrocytes (in the field of
vision), and an
*increase in the excriction of 17-oxycorticosteroids. Eosinopenia,
an
increase in excretion of products-of hormone decomposition,
indicated
the development of a stress reaction in cosmonauts. Since some of
the
indications found on the flight.were also found after training in
the train-
rd

-L 08269-67
ling ship, there is reason to attribute them to limitation of
motor activity
;under conditions of weightlessness. The functional shifts found
after
flight are indications of a general fatigue,. a moderate stress
reaction,
and a certain aniount of detraining''In general, the changes
observed in
'the cosmonauts were.of.one tM. The differences found between the__
cosmonauts can be attributed to individual differences. (W.A. No.
22;
ATD Report 66-1161
.SUB-CODE: 06p 22 SUBM DATE: OOMay66

L OSZ68-6i FBS-2~ ZWT( IjEEC(k) -21 SCTB
ACC NR, AT6036481
SOURCE CODE:
AUTHOR: Arzh )V. 1. M!j Dryanov, I. I.; Bal=vko, V. A.;
BerekQyRin, A. V.;
Buyanov -P. x6ii1eir.-V. V.: Kondrakoy M.; Krasovskiy,-A. 3.;
Kuzn
I - _ etSIDVA 0. N.;
Fe
Kuznetsov.-S. V.; Nikitin,..A._Y.; N
jgtrA" VtJ.,; 7~qrgtljev doroy Ye. A.;
Khlebnikov, G. 7. 6~~
ORG: none at-l
TITLE: Some reaults of the postflight Ipmination of P. I.
Belyayev and A. A. Leonov
following their flight on ttp - %pacocraft [Paper presented at
the Conference
hmw&~=
on Problems of 8pace MedicitflK eld in Moscow from 24 to 27.May
19661
SOURCE: Konfertintsiya po problemam kosmichetikoy meditsiny,
1966. Problemy
kosmicheskoy meditsiny. (Problems of space medicine); materialy
konferentaii,
Moscow, 1966, 36-37
TOPIC TAGS: space medicine, postflight medical examination,
bodily fatigue, body
weight, cardiovascular system, oculocardiac-reflex,
-unconditioned reflexo space
psychology,, oxygen consumption.. respiration, pulmonary
ventilation/Voskhod-2
ABSTRACT: Postflight examinations of the Voskhod-2 crew
members, Leonov
.and Belyayev, Were performed on the third and fow-th days
after the flight'
:and again a morith later. The cosmonauts complained of light
fatigued
They were found to have hyperemia of the mucosa of the nose and
thrioat
.and conjunctivitis of the eyelids and.ey~ballig. 71X7 had lost
weigh
TT/DD/GD/GW~

AC, C-, - -N, A, A T-6 0-3- -6-1 JI 3- 1-
Their pulse showe a certain labil ty. Pulse frequency ros'e
significantly
!during m.-Ad physical exertions and changes in the position of the
body.
,iThere was an ij.,icrease in intraventricular conductivity, "
increase in
;the systolic index (7-1116), and a delay in restoration of
hemodynamic
indices after physical exercise.
BelyayevI ;s oxygen consumption increased by 23% and LeonovI s
by 14% as compared with preflight levelsi Vital capacity of the lungs
diminished by 8-1276, while pulmonary ventilation increased by
51-1810.
'Neurological examinations revealed a light tremor of the fingers, a
high orthostatic reflex with an absence of pulse reaction to the
oculo-
cardiac reflex, and an increase in the slow bioelectrical activity
of the
brain cortex. :Psychological tests revealed an increase in
distribution
and in the middle magnitudes of the duration of the period of sensory
motor reactiom Since this was not accompanied by errors, it is
possible:
to assume that the fatigue observed in cosmonauts was a compensatory
reaction. Blood and urine examination on the third day after flight
did
not differ. substantially from preflight levels. Biochemical
examination
uncovered an increase of chlorides, adrenalin, noradrenalin, and
.17.-o,xycorticosteroids injhe..ur.ine.-.
Card 2/3

68-67
ACC NR: AT6036481
The observed shifts in physiological indices were short-term
and
reversible. They indicated the development of moderately marked
jatigue in the nubjects. Thus, despite the complexity of the
flight, the
postflight examinations revealed only moderate functional
changes in
the two cosmonauts. There was no difference in the nature of
these
changes in the cosmonauts. This indicates a high degree of
training
.and a good neuropsycholoocal and physical prepnrationfor
spaceflight.,
[W.A. No. 22; jM) Report 66-116]
SUB CODE: 06, ZI / SUBM DATE: OOMay-66
CoM 3/3

ARZHANOV, BMMR, G.M.
Cholesteatoma of the spinal cord. Vbponeirokhir. 24 no.6t43-44
)~-D 160. (KMA 14s1)
3.Orlmkaya oblastnaya bollnitsae
(SPINAL CORD-TUMORS)

IVAILIOVI ARZIIANOV, N.I.
Treatment of chronic suppurative processes in the lung
complicated
Irf metastatic abscesses of the brain. Khirurgiia no.10:119-122
164.
(MIRA 18:8)
:1. Orlovskaya oblastnaya bollnitsa (glavnyy vrach
M.P.Khrisanopulo).

ARZUNOV, P.
Solid shelves for storing mill p-.roducts. Ruk.-slev,prom, 2C no,6;
30 je 134. (KLRA 7:8)
1. luybyehevekaya realizatelonnapa baza Zagotserno.
(Plour--Storage)

E;'-.r,noriko-geor,.tiificlier,;dc osnovy S33A. ~.chcrld
i jruiter~aly. S rwilo',-honicn. "ablits: "ElconDn.-
icho.-Ide profili SSSR po raiLi;,wn Gospluall... Lunigrad,
Drol:gauz-~fron, 332
cty
&I- LC Soviet Gco~-,rapl~y Part t 1951) Uncl.

ARZRANOV, Ye.P# ,
W- wowwwwwww
Using light and shade to tontrol the smoothing of film.
Good. i kart.
no.1:24-27 J& 157. WaA 10:3)
(Photography-Films)

trol film
"It"r 'Aluc.---tion

AUTHOR:
w Graduate Stuient SOV/154-58-1-14/22
Arzhanov, Ypz
~

,
_
TITLE:
Checking the Level PassaCe of Aerofilm During the
FliGht

(0 kontrole vyravnivaniya aero-lenki v polete)
P
PERIODICAL:
Izvestiya, vysshikh uchebnykh vavedeniy.
Geodn:~iya t aero-

fotos,lyemkav 1958, Nr 1, PP 10-112 (USSR)
ABSTRACT:
In the paper under review the author discusses the
possabilitiez

of manometer checking of the level passage of
the filmstrip

during the flight. By neans of a manometer any
faults in the

evenness caused by some influence from th;
outaide could be

checked continuously. In the test the
oanometer recorded un-

evenness eighteen times. It waiii
caused from the outside

when small foreign substances I'micro
particle's) pcnetrated

underneath the filmstrip. In o';her
cases also other causes

of unevenness were dete,.-ted. The
test proved that the manometer

operated satisfactorily in the
course of the test and check..

ed any unevenness. All atages
of photography were tested and

any unevenness was recorded by
menns of a rastoir. The check-

ing method proposed may also bo
employed (iinder different
Card 1/2
conditions) in factoriea.
Thero are 3 figures find I reference...

SOV/ 154-50-1 -- 14122
Checking the Level Passage of Aerofilm During the Flight
1 of which is Soviet.
ASSOCIATION: Moskovakiy inatitut inzheneroir geodoz.1i,
acrofotoo"yehiki i
kartografil
(Moscow Engineering Institute of Geodesy, AerophotoCraphy
and Cartography)
Card 2/2

Irznanov, Ye. P., Graduate Student !;UV/ 1 "A --,84 -.41
On the Use of' 11neumazico-Mechnnical Means for VInt.toninn Films
in '.erinl Cameras (0 pnevmomakhanichenkom vyravnivanil
neroplenki)
Izvestiya vysshikh uchebnykh zavedeni.y. Geodeziya i
aerofotosllyemka, 1958,, Nr 2, pp 87-91
The introduction of the new aerial camera MA*M' resulted in
a considerable reduction of waste occurrjn8 in o ther cameras
because of the failure of the film to lie flat. Nevertheless.
work is still beingdone with a view to perfecting the metnod
of flattening-out films. Speoifically, the pneumatico-mechan-
ical method has been further developed. The basic idea on
which this method resti3 was developed in 1943 by Docent 4. T.
Shershen'. Essentially it consists of flattening the film by
mechenical means and at; the samf~ timp by a vacuum, wheretipon
the fluttening device -.'.s removed and the negative air presEture
is usea to keep the f-i.'.m in the right position. The first
systematic tests with regard to this method were carried out by
Ile. t~. Bugayets. These tests proved that this method made it
f'P. r di rossible to obtain a h4.gher quality of the film surfacf,
thnn

SOV/1';4-58-2-9/22
On ttio V::(! of Ineumatico-Mechanioul Menn-i for Flattening
Films in Aerial
Cbmoras
the ordinary pneumatic method. In 191*,6-57 the author te3ted
a
new device of Vio rollers moving in the camera casp. A sketch
of the device is attached. The testq proved that the frAction
ot' the rollers did not cause a frictional mint. The lab tests
-4cre carried out by T. F. 111ushtin, Candidate for the
Diploma,
and proved that the flattening of the film was carried out
more
effectively than had been the case with'the normal pneumatic
method. During 1956 and 1957 the method was also tested in
flight, and the results correeponded to those of the lab
tests.
The improvement is expressed in thousandths of millimeters. Tt
seems that the film is additionally "eaualized" by the move-
ment of the-rollers. !,till, the design will hardly be used
since the application is very diff:icult. There are 2 figures,
I table, and 5 references, 3 of which are Soviet.
A~')';nCTATION% tAoskovnkiy institut inzhenerov geodezii,
aerofotos"yemki i
kartografii kloncow Engineering Institute of Geodesy, '~ero-
photography, and Cartography)
Card 2/3

SOV/154-58-2-9/22
On the Ilse of Pneumatico-Meohanical Means for Flattening
Films in Aerial
Cameras
SITBMITTY.Dt October 18, 1957
Card 313

----------

A -I.

A.UTMOA.
Sol-shishov, V. D..
Candidate of Technical Sclaam.m

TITLXo
Smissuric &M Technical Conference of
XIXGA 1 9 (Y.,aam-

tekbalafteekays
komforentairs, all" I K) I

PERIODICALs
1S."Siya vyooblkh achobaylth savdonLy.
Camd.sly. t

1954, IF 2, Vp 111-114 (C=)

AB"MACTO

:lmtIfLc &ad technical aaeforence of
IF" April 24 to 26 a a

.ut
nl rA X Imat of Cood.sy, A.r.poatography.
ad
tb

Ca eamphy, Masao-) oas held in Masao..
F~rtavrwcre. there
;t

.or. tor toollons In 49,wrotical an
goo4soy.

*AF`94, and an the prodQation of
phatogrammetrital lawsr-

to. more than >00
delegates fro. 4$ so.tit~t" took part in

Ib. "aferude at which 2S leamures so"
gives. 20 delegates

pwrtiolw-d In she
dLeamselow. The opening a peach va,m me.
by

the Director of the K11CA 1 9. professor
P. S_ Zabotav. Doctor

et T_kmlml Sciences.
The first pop" read a- that by A. 1.

MWF "
-The Fight Lgaimt lolls lomkoa.~ A. 1.
Dwra0l.

'Tra-m.r, Dooter of Technical
Seltsites. d"k. .. 'ft. 3-t.p a 04

the
"welliag PrInalplow of the Coodstic Pasta
Notoork of the

1/3
UWE.' A. N. Lirav.ts.
Profammor. Food a paper " -Th. mamors-

t1a.
of Soso Kin" of God.tl"l

Directly mee..r.d
I. the

Ellipsoid .- R. S. *Ara--y-. Decent.
'On a Jonah Mark of

btlity.o T. 0.
S*JlkMnovtch, Doc"%, Candidate of

T_:: , Sol W" -The Life and Scientific
O.rk Of A. P.
=31 a I

Selassie." T
2- S-1-whakov. -optical X_Z~rowamte of

P1,eal . Couritions.. S. V. Toavlov. A 0 .
j
;
:

Z
at4platloso Z.~ W. to. Robir. -On the
Pro;lo; of Detimining

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goo. gimesto of 1m*i'OrlwmttLou or
md 3,:

:
:
wide A I* I.rial C"mrse.- A. K. Pilmew.
armidust ,.4 t,

On a A,
Mal Delta. With a Freely Sosp.ad.d
Reflector., AL. S.
I

Dialtriyam, reported on
*Goodway and Cartography at the 3*910-

AlAd
of ZUA Soviet 24-I..Iff.- r_Ayzh&_-- 2.
-in U-sellestle"

of t6.1112 Sssaothig
Deal*. uLtb 8~,,-Vgtatg '.. N.

Too Lk:y,
Gradvote Students -St.reaccuperster With
r4ectrical

herial. Des-L. C..41441. of
Tecftsi-I

seleme". "C'n the t:boj. or $..I.
of Aerial Pooto4raph. m".1t-

Img ?ran
to!argenvat.- I. V. Za"rovs -on to.
:18tiets..

C6pdnjlLtl* Of &cd Color
?ftQt*4rmPha.~ U. S.

to St.d..Ll -the Zl-t.
of the Theory of .
I :

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1
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State, or
Physical-Mathemat "I Kworl"g. - the
precise I.--
:

Us 104 of Soner1be ?sale.- 3. X. Colovi..
'$P-41.6 V and

lmp;:v,lod tho Prodactlas of
Mmsarq,4 Tools.- L. A. X!lkla.

Dscasm*,
Comildst. of Technical SeL.waom. -On
1-trum.at. far

Of ftstsncms.~ V. S.
SliLhoychow. An-
k

i:tmintl 71
!: Too&*With the Optical Range rlsder
CRS-1.6
:

'r. 9. usem. latent, *on the stody or
tnaoc.-.1- I. tn.
:

6 Plate" of N. Professor.
7664wel

Doctor f CoagraphItAl Sales.".
13coa, Avearse, a. Imm.ing in
:

St.. Production Prec.se of Original
Maps.-

card 3/5

ZAA A-N-TC V,-- I -_ - ---
niiTHOR:
None Given sov/ 6-58-6-21/21
TITLE:
Chroniole (Khronika)
111010DICAL:
Geodeziya i kartografiyai, 1958, Nr 6, PP. 79-80
(USSR)
ABSTRACT:
From April 24 - 26, 195EI a Technical Scientific
Conference

took place at the Mosoov, Institute of Surveying-9
Aerial

Photography- and Cartography Engineers (Moskovskiy institut

inshenerov geodezii, aerofotoe"yemki i kartografii).

In the
section of aerial-surveying the following lectures

were hold: N.
Ya. Bobir, Docent,- "On the Problem of the

Determination of
Elements of the Internal Orientation of

Aerial Cameras With Wide
and Superwide Angles"* Yes Pe Arzhanov

Assistant, - "Investigation
of the Apparatus for the traight-

ening of the Film by Means of
Waves" (compressed iromeohan-

leal Method by Docent A. I,
Shershenl~. V. Ya. Mikhaylov,

Docent, - "On the Change of the
Scale of Aerial Photographs

in the Course of EnlarglIng". L. N.
Vaaillyev, Aspirant, -

"Stereocompensator With Electric
Corrections". P. V. Zakharov,

Teacher, - "On the Fineness of Grain
of Black and White as
Card 1/3
Well as Color Negatives of Aerial
Photographs". Yu. M.

Chronicle SOV/ 6-58-6-21/21
Kuznetsov# Aspirantl - "Elemento of the Theory of the New'
Rapid Shutter".
In the section for eurveying and photogrammetric apparatus
the following lectures trere held: 1. 0. Sarkinp Professor,
"Physical and Mathematioal Theses of the Theorem.on the Ao-
curacy of the Apparatus as a Means of Measurements". S. M,
Goloving Docent, -OAccelerating the Production Preparations
of New Products and Reducing Their Costs". L. A. Malkinp
Docentp -I'Anvaratus for the &aot Recording of Diatances"o
Ve S. Nikboyesbo% Assistantt -4F:Leld Tests With the Light
Range Finaer CBB-1" (In Moscow -in August 1957)- V- S- Usov,
Assistant, - "On the Inveotigation of the Errors of the
Focusing Devices of Telescopes".
In the section of cartograpky the following lectures werq*
held: N. M. Volkov, Professor, - "On the Engraving iii the
Production of the Original Publicat~on Editions". A. V.
Naumov, Docent, - "Some Problems of t#e Household of Carto-
graphic Production". G. A. Ginzburg, Docent, - "On the
Inter-
relation of the Distortions in Cartographic Projections".
L. A. Bogomolov, Docent, - "The Topographic E`~ali~ation of
Card 2/3 Aerial Photographs Taken From Airplanes and
Helicopters in

~hroniele SOV/ 6-58-6-21/21
the Cartographing of Areas Diffieplt of Acceas", A* 3.
Tolstoukhov, Assistantt - "On the At,,presentation of Reliefs
of Plane Areas on Topographic Maps".
1. Cartography 2. Aerial photography 3. Scientific reports
Card 3/3

ARZHANOVO YE. P
Transactioup of the Ldboratory (ft*)*6 fA&rmmtbbcW j A& MLdff/3615
V.7j. Materials of 7th AU Interdept Confe Aerial Survey (Dec 56),
Moscow, 1959, 331PP.
Arzhanov Yit.P. [Moscow Institute of Cktodetic., Photogrametricy
Engineering].
New Methodis of Flattening the Aerial Film 102
Romanovskiy., G.V. INsuchno-issledovatellskly institut voyenno-
topograficbeskoy slfthby., SA - Scientific-heoearch Institute of
the Xilitax7 Topography Service, SAI,
The Pretent State and Pluture Prospects of Aerial Topographic
Surveying In the UNR 107
Rusinov.. XX. JLeningraftkiy institut tochnoy zekba-Ski i optiki
Leningrad ~:nstitute of Ptecision Mechanics and Optical.
New Wide-Angle Lensee for Aerial Plu)tography and Future
Prospects of Development 114
Zhakov., 0,:P, [Scientific-Research Institute of' the Military
Topography Service., SAJ.
Photogronmetric Apparatus 121
Card 5/15

TIT;X, ScI~=tlflc-t*ct-Ica% C.~f-'- ~.' t".
=I;A L X in
1959 (3L4'chw-%Gkhn-..beskAY& kzz.'v"ntml'.
=Nk 1 9 1359 S.,
Is."tLY4 ly..hil& -h-bAlkh 1 '-b
xes". 1939. Er 3. " 144 - 946 (=$a)
ASISTBACT. 2h. periodic of the
Inatit.9 g#o4.jjl. ..r.fotos-y.Ul I
krtOSftfil
(Moceco Ingtit.t. of Cood.tic. Aerial
Sur,ey and Cartographic
Engineers) One held On April 27-24, 1959
%be PAX11.1p.-
&I* of 500 persons. 31 ject.rem or.
d.1,':!r'sd. The Intro-
dac= speech a" hold by Professor A. A.
lzotc,. Candidate
at Philosophical Salesman I t 00 -Th:fg..%
macamms sari. r
-I.&1 $.is-- d. V. Loodrashkow On wA Goo-
dacjr~o CA"LAst. 0-. T. Rnarwl"I an
""a"I", of the 3 ,tie: of %be 1W.Ors*
?.sluom Compt.tio
With CoOrdi too ff rest Coodatle 3yoteme*;
Candidate a
..k.Leal sa`losaas~.F. Ft ShokLm reported
on -Crowlnotry in Cl-
Car& 1,6 1".Y.o Stage of V-.l.pmoM-j
C..Aldt. of Technical SOL.- as
id-tieft of the Sales "earning th .a
coacralizing the 4.11-f in photo-
S=Pkr*s post-Srduct. st.drat Tn. 1. Skb.,
ft 'Th. Iafl.._O
Of 9 X66"11-6 9-or ad the Lacraii Of
X6191-Me Of Linear
he
Sesseloo sy-tons . Pont gradecto StdAmat 1.
D~. Drox4o, roport.&
,on tb* SOI.tlom of LLowsr syntoOM Is
tki"GiRponsittiam of Go,.
"tie Se"'. Docomat dealt ItAl 'ft.
in tbO APJlIG&tIA`m Of ftrulLadtiO
?IlYI-OO-Otr7 With Shart
a-
_,. and e.-t"t Tortleal Somi... Doetar of
Mzsl.al ad math
MOSidel, S'lm-ac A. X. raynxillborg
lectured am ~Soa. Integral.
Fras th Th ry OT'Vur- -nr-TE Lr Application
to the Me
. as w -
sh.41- of Artiftlal S"-Sb Set.111too-I
C..dldst. of T-jml_l
Sr-I..'eve A. S. Taxeyce On -The
Stvroacesparator Xith Corroctars-.
poke on ~P%Otogram,.tri. Seth" of Do.
of L-LA~ Cie.".. Candidt. of Tach-
nical Sale-- ff- 1. report " 00 -the
a.-MIL24-
tLea of the Formalas for the PLO" &orlal
sorway and the Litt.
t-41461 As L.1 X%-vy'..Cs.4Iet. of T-hole.1
Sciences AL_j6_
2"I.Ove 89!~ Ca a Too 1.41
Zawa 't~' !!!!a!-!!
Ft" T'..
Seloosew I. W. NoIj .0. k. 0. the
'Stroboscopic Collimator Timor ro;artod
am O"Coertlxg Coor for Us Astocatic Entry
of the Alzplan*
18 the Aerial Pbotog"phy Path-.
Post-grad"to Stad.n% EA,_j.
Zass.t. spoke on the &A"1166%lon of the
Instantasooas Photo-
Srup for k.rL&I Camera " r-A
%ja:OatjagI. A..1.9..t
apok:Fou the of the A-rial Can.
ga4loser j,_L-AX%LLhAA, Chief Technician of
the GootakUmatom
00oplass, IMPS240-Soce I-Its and Task.
Rotated to Larg.-cal. j~b* t tb
"Ilt* 3~6TL-X Oporstleam-1 Sector of
Technical 301:=-
;jw~~ an -Th. Problem C...."LAd th.'c t
P . the Scal. of I . 2500000'1 Docto :11
:-clob.1cfallho
a. -Ki-ral Deposit. La the U331
amd ?b Lr so S-n0sla VAR--, A..I-t.-t
!L~vd-~ 1
_k23X-a: the -Wthod of 9*oIrspble le,o.
tigation a. the Field
bitrIng the Prn-Z-7 Ultorle Ifork on the
Crtographl.4
ObJect (YrO- the I-ftlag Zrporl..c. AOq.ird
by the U-b.b."-
kAY- -kwjl-dlt-LY- (XaaIcbsraItaY-
UpodItLOO of the KIICA I K _iq5e)
1-tOe" h--3 sit Ltb -The pirbl.. ~f La-
Ii.. graphic I#pr::ovtotLsn of , flat
Inhabited Torrit9r,
" the T!pd UP the Scale of I . 10000..
C..,u to
_LL,ft spoke an -Up. of Calti,.t.,
At
Areas 'a 'be CosIrrshossiv* Olactse of the
C..dIdat.
of T..halcal get---
dealt -itb 'A. 3. Pope,
t tz. ICC:b zl_-tb~&v Of
A. ff. Rep..)-. Senior letterer g I-etar.4
an
W~rar Zw Crbj:ctl-- Uth Great ideas
Lbt-ItY'- P"f4-*.r
X. G. s4r*t rep, 4 9. -Th. pr.bx - of
C..p.mmisting the Voris-
%I.- ad .h . or AaccrOcy, is the vas.~Qt or
pky_
oical rasatl: as. - C.'edlist. of ?Ocbmaal
Solen.- V. A.
F_AtA.!XKXdacIt -Ith -Ztb.4. or on ZOO-
ecralad C~Vttasl N*In Cheraft.rietLe. of
A.rI.l Con.rc obj.Otl,_
with Dropping Atcoarborl. pvsx-ro ad
I-P.-tars.. ZA&L.."
Inst-ca @a -urtical A.IA sy.t- of sigh-pre.
sislow 0pIjIaa2 Thaedolites-. L..jtmat
j,.AgV_9, &p.k:. a
-51aftuad by the Aid of 1.1"Oop- w_-tb Zen.
p"&_
47-don't Stedwst ?- dealt Itb -Th.
A.towntiou or
Gmr4 0-arecent. an . Fair of 3%.r--ple At
the pl._,,
Sdooloc h4ld a- kprll 24 tb* Chief Of the
CUT",- apravl*zlye
a-od"11 I kertogrfll an pSS& (Chief
Ad-laitratic. or asc-
4*-Y ned rartgraphy, Or the &,.ietrp or
1.%*r"l Aff.jr, of
the lacl._4 on -Th* sov.n-year plan and
the aseel.pao.t of T" 'hi.-good.tio $ad
Crtograot.

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RSA

ARZHLM)V, Te.P.
New method of tooting the flatness of aerial films. Trudy labs
aeromet. 7:102-106 159. (MRA 13r1)
1. Moskoyakly Institut inshanerov goodezii, aerofotos*yemki
I kartografit.
(Photograp)W, 4erial-,vlquipmont and supplies)

ARZMVOV, Ye.Pe, kandotekhnonauk
Computing the elements of inner oriantiLtion,
Trudy MIIGAIK
nci.39:57-62 160* (MIRA 13:8)
lo Xafedra aerofotosuyemki MoskovBkogo inatituta
inzhenerov
g(JOSM"i-serofotat"yeAlci i kartograf ii.
(Aarial photogrammebry)

ARZHANCV, Ye.P., assistent, kand,,tekhn.nauk
Testing the flattening of the aerial film by the usc
of its
reflecting properties. Izv. vys. ucheb. zav.; geod, i
aerof.
no.Z:111-117161. (MIRA 14:6)
1. Moskovskiy Institut inzhenerov geodezU9
aerofotos"yemki I
kartografii.
(Photography--Film4