SCIENTIFIC ABSTRACT TIKUNOVA, YE.I. - TILEVICH, I.A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001755620020-3
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: July 16, 2001
• Sequence Number: 20
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

TIKWOVA. Ye.I.
CandidAMraotic plemritio. Sov.med. 23 no.7:83-84 -T1 '59.
(KIRA 12:11)
1. Is propedaytichookoy terapovtichookoy kliniki (save - prof.
S.V-Sheotakcv) Xijybyehavokogo maditainakogo Inatituta.
(MCHILIASIS)
(FLNMSY)

ACC NRo AP6021572
SOURCE CODE: UR/013V66/000/003/0059/00'61
AUTHOR: Nazarenko, N. D.; Vlasko, N. I.; Tikush, V. L.; Scryabinskays, L V.
OMR Institute of Materials Researcho AN U`krSBR (Institut Problem Materialovedeniya
TITLE: Buporduty nonfired refractories with magnesium phosphate used as the binder
SOURCE: Ogneupory, no. 3, 1966, 59- 61
-TOPIC TAGS: refractoryl magnesium compound, phosphate, nonclay refractory product
ABSTRACT: Superduty concretes were experimentaRy produced on using fused-magnesite
wastes of electric-beater production and monosubstituted magnesium phosphate. The phosphate
was obtained by adding small portions of active MgO to preheated phosphoric acid:
Mgo + 9H 3PO 4 _* Mg (H 2 P04)2 + H20
and evaporating the solution until a dry residue remained. This residue, dry monosubs
magnesium phosphate, was added as the binder to the charge. Specimens of the resulting ma-
terial were immediately pressed In semi-dry form in a hydraulic press and dried, first *in

ACC NRs AP6021572
air and then at 100-110'C (when the final setting of the phosphate binder additionally enhanced
the strength of the material). The dry specimens were heated to 900*C in a muffle furnace
and to 1700'C Ina Kryptol furnace. Findings Indicate that the minimum! 'pallingro-
-sistaice of the specimens after heating at 900*C is sufficiently high, aDd that It increases
markedly when they an heated at 1200-1500"C. The material thus developed may be primarily
recommended for the production of rammed refractory linings and accessories (including
flame tubes) for h1oh-temperature furnaces of the laboratory type; Orig. art. has:. 6 tables*
SUB'CODZ: U SUM DATE: -none/ OTH REF: 002
4
2/2
L Card

TMKVBWSXI, S.
Affirmation of the Electrical FactorT OJug" on domestic and foreign
markatB. Elektroprivreda, 11+ no.7/8:1+01-/+03 .11-Ag 161.

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tals do not corrutle was veritted on a munple Ali
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pulified Zn, A slight coritwitiss, of 7a in W5 X
f
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I!CI tooli place only at breaking avvinlq, or victatelim
kovtotunt (III ottlinary Zn was different in ilifferent mattipli,q.
ml o ..well rbal'It"I on puli-hing ov. I flit, -tatin, -dolpIc,
III ull I Is- 4.11. 1 all Instant twil-1) 0... 4w vr~x 41% w.1,
Ulicit /%I wit% coconvUll It, oil 0mtf'%t'. .4 .4 dif -
I,frtll flit 141 c.411ainvol in the *mine mills. tilt
voric.-Ity incitru."I while tlw still. .( It fet,.Iv"l '", /11
J., 1. a-I .'bffrf.Iw.- rol-ft I . The vahl. .4 she 1110'.1, it,..
rfl"'I WI11% 11CO;kOfflosal W OW rnflefIl 110111PInit In tilt- r$t
fiscal. This is tritplained ivy the inctrav of the concti. %I
too Zu in the contact layti of the soln- ithich was cauwd Ivy
inctreased Wn. of Zn, and which was countirtevi with the
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P (K4. In alkali) the difference effect Is Ititer than for In.
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: When di-"nlvrd its lICl the difference effect of Al it till.
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atinit strik," of arst hilt on the soln. of In cannot tic cii-
planted by licit ovirrvollatir of It Ill graphile, since tbi~ 1%
If of lilt **flit oldet of Illagnillidir as sisal I)( Ilb.
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AID lgr. 990J-6 14 juae
SC~ENTIFIC -TECHNICAL CONFERENCE ON MODERN GYROSCOPE TECH-
N9)~,OGY (USSR)
Izvestiya vysshikh uchebnykh zavedeniy. Priborostroyeniye, v. 6, no. 2, 1063.
156L.158. S/146/63/OOG!002/010/010
I
The Fourth Conference on Gyroscope Technology, sponsored by the Ministry
of Higher and Secondary Special Education RSFSR. was held at the Leningrad
Institute of Precision Mechanics and Optics from 20 to 24 November 1962.
The conference was attended by representatives from 93 organizations in
30 5: cities, including educational establishments, scientific research in-
stitut..i, design bureaus, and industrial concerns. The following are some
of the topics covered in the 92 papers presented and discussed at the conference.
Vibrations of a gyroscope pendulum with a movable suspension in a nonuniform
gravitational field: M, Z, Litvin-Sedoy, Senior Scientific Worker: improving
dynamic characteristics of some gyro instruments and devices: A. V. Reprikov,
Docent, Candidate of Technical Sciences; some problems of:the dynamics of a
gyroscope with an electric drive installed in a gymbol suspension: S. A.
Card 2/3

AID Mr. 990-6 14 June
8CnNTInC-=CET=L CMWEMCE (Cont'd) 6/146/631006/002/010/010
kharlamov, Engineer; problems of the theory of theInertial method for measur-
ing aircraft acceleration: 1. 1. Pomykayev, Docent. Candidate of Technical Sci-
ences; determining the drift of a floated-type integrating gyroscope without the
use of a dynamic stand. G. A. Slomyanskiy, Docent, Candidate of Technical
Sciences: natural damping of nutational vibrations of a gyroscope: :U__Y__0uIsv
Engineer; motion of a not quite symmetrical gyroscope pendulum with vertically
movable support: A. N. Borisova, Aspirant; gyroscope-type inclinometer for
surveying vertical fr'eezing wells: V. A. Sinitsyn, Candidate of Technical Sciences;
effect of joints between channels in triaidal gyro-stabilized platform: L. N.
Slezkin, Engineer-. theoretical proposal for the possible design of a generalized
gyro instrument: M. M. Bogdanovich. Docent. Candidate of Technical Sciences;
problem of drift in a power-type tria2dal gyro stabilizer: V. N.' Karpov, Engineer;
methods of modeUng random disturbances in gyro systems: S. S. Shishman, Senior
,PngLneer; method of noise functigns for investigating a system subjected to random
Card 2/3

Alv xr. 990-6 14 Tuns
SC:~N=1C-=CM=L COMr.== (CMt 'al S/146/63/()06/002/010/010
sigbals: G. P. Molotkbv. Docent, Candidate of Technical Sciences; drifts In a gyro-
st4ilized platform as a result of the effect of cross joints under determined and ran-
dom disturbances: B. 1, Nazarov, Docent, Candidate of Technical Sciences-, stability
anq natural oscillationsin Inhomogeneously rigid gyro systems with backlash under
external in' fluences: S. A. Chernikov; methods of designing a gyro vertical with
aut6matic latitude and course corrections: A--Y- _T111,_Candidate of Technical 9clen-
cep: use of asymptotic methods in solving problems of the motion of an astatic
gyroscope in gymbol suspension: 0. M. Klimov, Candidate of Physical and Mathe-
maiical Sciences, and L. N. Slezkin; theory of aperiodic gyro pendula: V. S.
Mochalin, Docent, Candidate of Technical Sciences; and selecting basic parameters
of course gyros by uking nomograms: V. P. Demidenko, En&eer. [AS)
Card 3/3

TILI, A. V. (Candidate of Technical Sciences)
"Methods of designiag a gyro vertical vith external influences"
report presented at the Scientific-technical Conference on Modern Gyroscope
Technology Ministry of Higher and Secondary Special Education RSFSR, held
at the Leningrad Institute of Precision Mechanics and Optics, 20-24 November 1962
(Izv. vysshikh uchebnykh zavedeniy. Priborostroyeniye, v. 6, no. 2, 1963)

-T-,/ (' ~-. ii - V -
WZIHINI V.11, dote., kand. takhn. nauk; B=KHOV# N.A., inth.; T11', A.V..
insh,
ALS-1 instrument uned for locating faults in commnication lines
having steel and nonferroun metal viring. Sbor. nauch. trud. LVTIIZHT
no"5:118-132 153. (MIRA 1113)
(Riles techniques (Blectronice)) (Rai lroeAs-Communication aystsm)

TILI -.), B.L.; SUSLOV, V.P.
Mechanical welding of the axle shaft housing of the ZIIP-157 automobile
Avt.prom. 27riD.6:37 Je 161. (MIRA 14:6)
1. Moskovskiy avtozavod imeni Likhacheva.
(Automobiles-Weldina)
0

I . MAMSHINA. I.; SAPUNAR, K.; PONOMAM, A.A.
lj~" I -
Study of furan compounds. Part 7: Two-stage hydration of furfuz7-
lidene ketones. Zhur. ob, khim. 27 no.1;110-117 Ja '57.
- I - (KLRA 10z6)
1. Saratovskiy gosuclarstvonnyy universitet.
(Paraldehyde)

PONOMAREV, A.A.; TILIt Z.V.; SEDAVKINA; V.A.
Furan compounds. Part 253 Dehydration of furan and tetrahydrofuran
alcohols and synthesis of furyl- and totrahydrofuryl alkanes. 7,hur.
ob.kh1m. 33 no.12s3951-3954 D 163. WIRA 17:3)
1. Saratovokiy gonudarstvonnyy unlvori)itot linoni Chornyahovskogo.

WIRIT-Mis TIAMW~iltkMNII-IeP:~, ll~i -- - - -
-1 . I
_-r- - - 1., %
I - tt

TIL', Z.V. nc.-, Sci. -- (di;!:0 11Jynthe-.-,!-:-- ,,nd catalytic
converaions of secondary and tertiary Puran alcohols and t~*-e-ir
derivatives." Sax-atov,1957. 19 PP 19 cm. (Min of lii~-,ber EdaceLtioll USSR.
Saratov State Univ im Chernyshevskiy). 150 copies. (KL, 23-57, 109).
i

-'~- I'L") ~ V
I-/-
USSR/Organic Chemistry - Synthetic Organic Chemistry, E-2
Abst Journal: Referat Zhur - "JIdYa., No 19, 1956, 61529
Authors Ponamarev,, A. A.,2-ill-4 _Z_V_
Institution: None
Title: Synthesis and Dehydration of Tertiary Furan Alcohols
original
Periodical: Nauchn. yezhego#ik za 1954 9., Saratovskiy un-t., Saratov., 1955,
497-500
Abstract; By interaction of 2-acetylfuran or 1-((x-furyl)-alkanones-3 or
-5 with Mg-alkyl halides bave been synthesized the-tertiary furan
alcohols: M 0 - 8%)ncoff(CH )R_(I) (listi n' R, Yield in %,
BP in 0 C.9 a :0) C6H5(lai -50 112 116~021 1-5558, 1.1220;
00 C4Hq' 2 o6., Lqe43; 0, iso-C5H11, 43, 81-
59j, T-7l -5, 1.47 -
82 .5/2.5, 1.4679, o..9648; 0, CH2C& 58, 123-124/3, 1-5340, 1-081;
2; C2H5: 72, 81-83/2, 1-~787, 0.9942; 2, C4119, 63, 114-116/3-5,
1.4-746., o.9683; 2. k1" 55: 130-132/7, 1.4730, 0.5$75; 4, CH3,
64, 96-98/2-5, rf!.~c 4 1, in which n = 0, were dehydrated
1.47 ~ 0.997 -
Card 1/2

USSR/Organic Chemistry - Synthetic Organic Chemistry, E-2
Abst Journal: Referat Zhur - Xhimiya, No 19, 1956~ 61529
of J ; other I were dehydrated by pataing their vapors at 220-
AR5-10 mm through tube containing aluminum silicate catalyst;
thus from Is was obtained 1-(cc-furyl)-l-phenylethylene, BP 105-
lOrIO/2 mm, n20D 1.5770, d2o 1.086; in other instances were ob-
.H4 -(CH2)n-C(CH CHR (listing n, R. BP
tained a es C4 30
0 CI n2q;"Idl~keno C3H71 72-74/15, 1.4940, 0.9273; 0, i8o-c4.Hg
Z'
(II), 92-~*/11, 1.4;10, 0.9122; 0, C6H5, 131-133J5, 1.5986,
CA, 91-94/8, 1 4720y
2 cH 65-67/8, 1-4735, 0.9222; 2, .4720
O'.9~33 47; 2, iao-C4H(?, 98-1C?31~, 1.4705, 0.9017; 4, C 31
8o- 778~, 1-4717, 0-9121- 11 was hydrogenated in alcohol over
PtO (activated FeSOU) to 2-((X-tetrahydrofuryl)-5-methylhexane,
BP 93-5-85-50/10 mm, D20D 1.4390, d~o o.8498.
Abstract: with 60~ yield by short heating to ' in presence of a crystal
Card 2/2

461
AUTHORS: Till, Z. V.; Markushina, I.; Sapunar, K.; and Ponomarev., A. A.
TITLE: Study of Furan Compounds. Part 7. Two-Stage Hydrogenation of
Furfurylidene Ketones (K izucheniyu furanovykh so edineniy. VII.
Dvukhstadiynoye gidrirovaniye furfurilidenketonM
PERIODICAL: Zhurnal Obshchey Khimii, 1957, Vol. 27, No. 1, pp. 110-116 (U.S.S.R.)
ABSTRACT: The authors describe the results obtained during two-stage hydro-
genation of several furfurylidene ketones synthesized with a yield
of 60 to 86% during the condensation of furfurole and homologcus
ketones, namely: furfurylidenemethylethyl ketone, furfurylidene-
methylpropyl ketone, furfurylidenemethylbutyl ketone, furfurylidene-
methylamyl ketone, furfurylidenemethylisohexyl ketone, furfurylide-
neacetophenone, furfurylidenepropiophenone and furfurylidene-
benzylideneacetone. The furan alcohols obtained were hydrogenated
over kieselguhr catalysts and converted into tetrahydrofuran alcohols.
The secondary reaction products obtained were identified as alkyl
and aryl homologues of 1,6-dioxAspiro (4,4) nonane. Tables 1 and 2
offer data about the most important physical constants and analyses
Card 1/2 of all products obtained from hydrogenation. Pressure hydrogenation

461
Study of Furan Compounds
of furfurylideneacetophenone and furfurylidene 0propiophenone in
dioxane as solvent and Raney's Ni at 135 - 140 led to immediate
hydrogenation of the furan cycle and elimination of the carbonyl
oxygen. Experimental data are presented showing that the condensa-
tion of furfurole with methylalkyl ketones results in the forma-,
tion of furfurylidene ketones of normal structure. The properties
of a liquid product obtained from the alcohol-phenylisocyanate
reaction were not investigated.
Two tables. There are 30 references, of which 8 are Slavic.
ASSOCIATION: Saratov State University (Saratovskiy Gosudarstvennyy Universitet)
PRESENTED BY:
SUENITTED: February 14, 1956
AVAIT-AM
Card 2/2.

PONOMAREV, A.A.; SEDAVKINA, V.A.; TILI, Z.V. -
Furan compoqnda,, Part 22: Influence of the structmre of-~fux7l-
all(anols on the reaction orientation during their c4talytic
hydrogenation, Zhur.ob.khim. 33 no.4:1303-1309 Ap'f63.
. - (MIRA 160)
1. Saratovskiy gosudarstvennyy universitet imeni N.G.Chernyebevokogo.
(Furfuryl alcohol) (Hydrogenation)

PONOMARIV, A.A.; jjk:aJWJ&; FISHMONOVA, A.D.1 RESHBTOV, V.P.
Study of furan compounds. Part 9: Synthesis and hydration of
tertiary ( -furylalkanole. Zhur.ob.khim. 27 no-5:1369-1374
my '57. (HLRA 10:8)
I.Saratovskiy gosudaretvannyy univereltet.
M=an)

."S 11-1

"ONOY
ARSY, A.A.~ - ~TI L 1~2 V
study of furan compc-.1--dr, Part 8: Solectiva hydrat'on of the eth7l-
ene bond of A -unwtuisted. fumv mildohydes and kotones in tbo
presence of Pady's -.--,^kel -atalvat. Zhur. ob. 'Thir, 27 no.4:1075-
10?8 Ap '57. NIYA 10: P.)
1, Saratovskiy ga~udztrstvermyv univervitat.
(Puran)

Di n tr, vIn hydr,~genfalcm af
J-]R M3
M
~Up K"-fA-

A A Pontonarvt Z V TH, A LIP "U-k r as"
11-13, --Tr'
'I 'T ("It
,'I, JI'( if"Ou IAAl j, i'~fj j
~e "k -II. ~ r
ii Al Iti
wc~c cbtaiacd in tt~-, ial"trd yields Lfter fractioiLation.
R shown): Ef, b'j 102-4', 1 4443. 0 9414 (23-71' Pr,
1.4466. 0.94~,~ Ba. b" W-10i, 44()a.
f131,YJ (41 317, ~; mq-Ru, 1,,a (0 V. 1 4470. 1J 93-40 14 3 J.
--.1 -, " uJ7 5 v 4 m" 9 TW~I ('54011, it Ik
-4mity El. L,,-. I 14
i.!~~ JI '. I 4o2-~~ a ~45.1 I

PONOKMV, A.A.; TILI, Z.V.; MARKUSHINA, I.; SAMIAR, K.; MKSTAROV, A.N., akademik,,
Maltistep hydrogenation of farfarylidene ketonee. New homologs of 1,6-dioxaspir
(4,4)nonane. Dokl.AN SSSR 93 no.2:297-300 N '53. (nu 6:10 01
1. Akademlya nauk SSSR (for Nesmeyanov). (Hydrogenation) (Nonane)

PONOMAREV, A.A.; TILI, Z.V.
Faran compoands. Part 27~ Synthesis of Bome
2-(2'-furYl)-1,3,4-oxadiazoles and fu--oylhydrazones. Zhur.ob.khim.
33 no.7t2368-2372 Jl 163. (MIRA 16:8)
1. S4atovskiy gosudarstvennyy universitet imeni Chernyshevskogo.
(Oxadiazole) (Hydrazones)

VdpW bOoM d ift SMS MiM A. A. Pm"w-. L.
mW V. V. Zekslow" CL14". USSR. 1960. A A51-a
(U'S. .W., 1127-11 amowstal &Mobydm candsom
WhK &Ikyl. alkyloyl. &at hotarmyrije owthyl ketnow. wMng vxid
of the Comeponding dl-, tri.. arml tetr"no kvttmwo. 110
moot t ad polyetw kator" of the furm
formed by the tka ON 0~-r-fuvylokcrvarln with
b"0 batow, owthyl 0=71 nd yrryl tor4hyl
0'.
of 1-21-fadur at With ; h 'phonons,
with PjsAC4*W. Met toomnyva =#.~wthylbeuclybvwne.
WAyl botow. IW Inns klen-
For t botomm wikb sjrphu.
gwt~uit with cow- 11's0,. tic , cc
All Ow pedywoo am by asima a I : I -mokr fado
0 . or furyl-
imkb beftbomm Ki of
10% Nooll. witk 0 ow om-qbm 12.
4 , wAwA%Yhw"-l -& 3 : A*dW?-Vw. "t, P.
INIP (2 , 4400*4`00,00"01W.
1-r
3w vt soxyl tow VI
;1,;~ OL S,
log 43%), M.P. 63,
NMI T give I
isib 00"" "nowl- W.- - -1 ..,1- .... 91.
;,~f Wj. 107zlolp a.

:-4-
: 4.
A to
900A
of the

Seses petiltne ketones of
00"Wry. Z, V. TO. an', V. V
ShIV S(Att LVIV. ' FLU4VIV). Zkor. OlIjAcAd Kh
r,.w. Chem.) 20. PIZ W(JOW).-Fursti-biasitill
sidehydes fC*(Iily FVACt with hie ketones end yi
tri-, and tetractir ketones. Z-Forawacraleva was
by Kiluitt's method j C.A. 20, 123S) in 72.5% yiel
-3* reaction temp. anti 3.6 hrs.' duration wert
imal was also made according to Xonij
pvrl~s _Wsdrxe)prep-j*e was prepl. from furfu
14 1 rFfvCri3
HtC JO according to 1). Ivantsv (CA. 19. 1138
C
following ketolles % etc litclid. analogously by Conde
U the above littones vnth RUINIt sm &q. a6. with 1(#%
NaOlf. A typical examplez 4 g. 2-furtinacrolein and 6.6n
CjfjpCO1Ie In 25 ml. 70% EMU with 4 mi. 10% %'&-
t
Ii pvt In 24 firs 46%
ister. in, 63* (from in.
95-61. Other ull Ould, I - U -flopyl)JI josqNs Inelvd,
(M.P. of in partsithesest in.
cluded: 8.11 -dist.FlAyl - 1.3,5 - 1104,11WIS - 0. - 041. M. 926.
(136 7*) in fill '- yivl,l;
m. W. (210'~; I..? - heird.,tadiew ..', -one. in. 50-M
(124-S"); on,, pit. 79' 12X V);
1.3.7-Atxd4eirdto ten -7 in. lit * It I V 12') ; 7-phrnyl-
sit. MI 7- xi-,* ii oren
color with Z .,"elk v/. 1,1 -p-i ladies ..' -on t,
M. 107--H* 1170-l't. give. Is r4A , for with 11,;0. sn'l
conol. 110; in. 110-
20' OU-S"). gives a brown color wall 11,SAP.; 7-jsAeqyi-
I
in. 141-110" (A '), vioirt
in 11,50it. turning yclNm (pi diln.:
deep-red, with concil. IICI A blux-Creen color; 5-(Z-p)r-
lit. 156.5' (21V), red.
brown in 11,50., ted its 110, swl rc.1 in fir-Cl(U: 54.1-
pyritmeth 1 -.1.3 - prooNdien ;.one. in. 171'
red-jarowis r.1 in )ICI, yellow in 10-010,;
in. MI* (2rwtfj*),
bitown-red In red lit 110. drep r"l in lit-CIICL.
The yk-kis from ',Jltqiti%,rr Oil';. with few
Cams In the 4")" cinitc. 6. M. Ku.01AINA

TILA, YUOPI, Cand Agr Sci -- "Certain problems of the jo4*4&o
1 0
i I i, ~ b to;..)
agricultural enIn er
ti e g, on light soils." Kaunas, 1961.
(Min of Agr USSR. Lithuanian Agr Acad) (KL, 8-b1, 25.11)
- 386 -

TILAJKA, Sandor
Ela3tiC loom propilsion. Magy textil 17 ro.1:3-'7 Ja 165,

CEHLINA, A..3 LASIS, A,~, SWDS. V.;-I.ILAYS, s.; im'AITU, E.;
All'. -~"IF-75'- 1-'-'FdRXLINS, J.-
KELPIS, E. -, S ;ANIS, A- ttEif 1 6 0, 1.
ABOLINS, J.-, KULA, F~ TIMSANS, S.; JESMINSI.-L.3
FRUSIS~.R#- KIAVINS,, E., rqdo
(Overall moc-banization. ,:~f dairy farms] Piena lopu farrrru
kompleksa mehanizacaija. Rigav Latvijas Valsts Izdev-
nieciba, 1964, 309 p. [In Latvian] (MIRA 18-7)

SHMIXAN, H.K.; ANMETEVAJ I.A.; PALENKO, I.A.; KOSITSM, I.Te.; TILIBA,
__A,P,4_RARAHCHZTSV, L.M.; MOSKAIJMO, A.T., red.; G(LOVIR, A.A.,
takhn.red.
[Nature in Amur Province] Priroda Amurskoi oblasti. Blago-
veshchensk, Amirskoe knizhnoe izd-vo, 1959. 308 P. (KIRA 13:4)
1. Amrskly otdol Tsesoyuznogo geograficheskogo obahchestva (for
all, except Moskalenko. Golovin).
(Amur Province--Geography)

TILIBA, A.P., kand.biologicheskikh nauk
Bottom-land vegetation of the Amur River. Amur sbor. no.2:151-10
16o. (MIRA 15:3)
1
1. DeystvJ*ollnyy chlen Geograficheskogo, obshchestva SSSR.
(Amur Valley--Botany)

, ~, . 73 . "and. ;7Iol--F,. -c1.
i IL I BA r% L w
Dissertation: "Effect of 'Nitrogenous fertilizers on the 6rowth and
Yield of Soya." Moscow otate Pedagogical Inst imeni V. 1. Lenin,
27 Oct 47.
SO: Vechernyaya Moskva, Oct, 1947 (Project #17636)

TILCHFTV, M.D. I
A. N. SAKIIIANC)V, Gonu(larstvennne Natich.-Telcri. lz,-Iritplstvo
Toscow-potro rad 1931,18-79.
"
I

Genera r -u i at 1 0- t"'e JPV'
'21
new theory Cf ~he ~encral Ci ton OT
ABSTRACT: This paper dtscg:~ses a
re which Is based on the law of rotation of particles (layers) of a heavenly,
of syme'~ ry The the-ury retogntzes the fact that the stratt-
~Osphe
cart1cles to ~he
Q
M
r
PLO
ME
WN
00, _0

W
L 10,~92 -65
ACCESS I Ot4 NR: AP4045510 f'orecasti ng
MS '5 Uh
ej
3rt. has- 5 rOrlm"
ON
OT
kin !l5r S0,4, mc-

TILE, G. [Tile, H,], prof.; BMBOM, P., doktor (Berlin)
Prevention of allergic diseases. Hauka i zhyttia U no.5:42-./+3.. 46
my 61. (MIRA 14:7)
(AIIMMY)

.00WITRY USSR
CATEGORY Farm Animals. Q
General Problems.
ABS. JOUR. RZhBlol., No, 61 1959, 110. 25767
AUTHOR :-Tile, I,; Pshanichnaya, V,
1.703T. scow Academy of Agriculture ineni K, A.*
TITIX- :The Application of Antibiotics in Feeding
Young Fowl and Nursing Piglets.
OIRIG. PUB. :Sb. stud. nauchno-issled. rabot Mosk, s.-kh,
akad. ~m. K. A. Tiziryazeva, 1957 (1958) vyp
L
t
16
i
ABSTRACT vea.
s were g
/ months old pulle
ng
:When Z
of penicillin with their feed, their voight
gains increased by 10 percent and the expendi-
tures of digestible nutritive substancos were
23.3 percent lower per 1 kg of weight gain
than in control young stock and correspon-
l
ets whick were
dinglyq the figures for pul
each given 24 mg of penicillint were.5 and
18.5 percent. The egg production of the
latter group was 220 percent higher, and
CARD: 1/2 *Timiryazev.
**7t 150-156

U OU'-J, TRY
CATEGORY
ABS. JOUR.
AUTHOR
DtIST.
TITLE
ORIG. PUB.
ABSTRACT
USSR
I FLZ,,jj3joj., No.
19159, Plo.
of hens receiving 16 mg, 73 percent higher
than in controls. Wben piglets were given
3 mg of" penicillin during the lstj 6 mr, during
the 2nd7 and 10 mg during the 3rd 10-day pe-
riod per head, their weight gain was 17 per-
cent higher than in coratrols, When antibio-
tics were given to nursing piglets sick with
diarrhea, the disease process was terminated.
It is recommended to use penicillin waste. --
Me F, Demina
Card: 2/2

---TILEI J.
Tvmortance of inhibitors in the fight against corrosion, p. 256,,
TEbMICKA PFACA (Statne nakladatelstvo technickej literatury)
Baratialava, Vol. 7, No. 6, June 1955
SOURCEs East European Accessions Lierb (EFAL) Library of Congress.,
Vol. 41 No. 122 Decedor, 1955,

GARBUZOV. Andrey Igaatlyevich, doteent; NISH-11, Tasiliy Porfirlyevich,
doteent; THJ, Vera Xarlovna, assistint; KUTSHINZIT, M.N.,
red.; Z6rd~.-Jrr . -ekhn.red.
[Somimicro qualitative chemical analysis] Xachostvennyi
khimichaskii polumikroanalis. Moskva, Goo.izd-vo med.lit-ry,
1960. 230 p. (MIRA 13:5)
(Chemistry, Analytical-Analitative)

7 IL
PHASE I BOOK EXPLOITATION SOV/4288
Garbuzov, Andrey Ignatlyevich, Vasiliy Forfirlyevich Mishinp and Vera Karlovna Tile
Kachestvennyy khimicheakiy polumikroanaliz (Chemical Qualitative Semimicroanalysis)
Moscow, Medgiz, 1960. 230 p. 20pOOO copies printed.
Ed.t M.N. Kuvahinskiy; Tech. Ed.t N.K. Zuyeva.
PURPOSE: This book is intended for students of chemical analysis at medical schools
and institutes for stomatology.
COVERAGE: The textbook., which reflects the academic program in qualitative semi-
microanalysis outlined by the General Chemistry Department of the First Moscow
Order of Lenin Medical Institute imeni I.M. Sechenov, covers the theory of
qualitative semimicro detf:mination of the chemical elements or compounds con-
stituting a substance or mixture of substances. Both chemical and physicochemi-
cal methods are discussed. The first is based on "analytical reactions"
(characteristic reactions) of certain reagents while the second is based on the
physical characteristics of the determined substance, e.g., absorption spectra,
shape and color of crystals, the nature of luminescence under ultraviolet light,
malting point, capacity for adsorption on various adsorbents, etc. The text-
book also reviews chemical methods of analyzing inorganic substances. The
authors thank Professor Ya.S. Przheborovskiy and N.D. Verderevskaya for assist-
Card 1/ 10

Chemical Qualitative Semimicroanalysis SOV/4288
ance. There are 39 figures and 4 tables. There are no references.
TABLE OF CONTENTS:
Foreword 3
Introduction 5
1. The subject matter of analytical chemistry and its significance in
science and practical applications 5
2. Methods of qualitative analysis 6
3. Main stages in the development of qualitative analysis 8
PART 1. THEORETICAL PRINCIPLES OF QUALITATIVE ANALYSIS
Ch. 1. Basic Concepts Concerning Solutions 10
4. Solutions and the concentration of solutions 10
5. Solubility and factors on which it depends 14
6. The law of distribution 17
7. Colloidal solutions 18
Test questions and problems 20
Card 2/ 10

Chemical Qualitative Semimicroanalysis
SOV/4288
Ch. II. The Rate of Reaction and Chemical Equilibrium 20
8. The rate of reaction 21
9. Dependence of the rate of reaction on the concentration of rea-
gents. The law of mass action 21
10. Dependence of the rate of reaction on temperature 22
11. Irreversible and reversible reactions. Chemical equilibrium 23
12. Shift of chemical equilibrium and Le Chatelier's law 25
13. Shift of chemical equilibrium with the change in concentration of
reagents and change in temDerature 26
14. CondItions under which reversible reactions are carried out to near
completion 28
Test questions and problems 29
Ch. III. The Theory of Electrolytic Dissociation and Ionic Equilibriums
in Solutions of Electrolytes 30
15. Principal premises of the theory of electrolytic dissociation 31
16. Types of chemical bonds 32
17. The mechanism of electrolytic dissociation. Hydration of ions 40
18. The degree of electrolytic dissociation 42
19. The ionization constant of an electrolyte 44
20. Principal premises of the theory of strong electrolytes 45
Card 3/10

Chemical Qualitative SomimieroanalyBis
Test questions and problems
SOV4288
48
Ch. IV. Acidst Basesland Salts 49
21. Acids,, basesoand salts 49
22. The reaction of a medium [i.e., water, its ionization] 54
23. The hydrolysis of salts 56
24. Amphoteric hydroxides. Ampholytes 58
Test questions and problems 60
Ch. V. Theory of the Formation and Dissolving of Precipitates 61
25. The solubility product 61
26. Formation and dissolving of precipitates 65
Test questions and problems 68
Ch. VI. Redox Processes 69
27. The essence of oxidation-reduction processes 69
2C. Oxidation and reduction 70
29. Redox equations of reactions 74
Test questions and problems 77
Card 4/10

Chemical Qualitative Semimicroanalysis
SOV/4288
Ch. VII. Complex Electrolytes 78
30. Complex ion formation 79
31. The stability of complex ions 80
32. The value of complex salts in qualitative analysis 81
Test questions and problems 82
PART II. THE EXPEFLIMENTAL PART OF QUALITATIVE SEMINICROANALYSIS
Ch. VIII. The Technique of Qualitative Samimicroanalysis 83
33. Organization of the working area 83
34. The technique of carrying out important operations 87
35. Conditions for producing reactions and the technique of providing
these conditions 94
Analysis of Cations
36. Introduction
37. Clasaification of cations
97
99
Ch. 11. The First Group of Cations 102
38. Characteristics of the group 102
39. The value of compounds of the first group of cations in medicine 103
Card 5/10

Chemical Qualitative Semimicroanalysis SOV/4288
40. Reactions of potassium cations 104
41. Reactions of sodium cations 108
42. Reactions of ammonium cations 109
43. Reactions of magnesium cations 112
44. Analysis of mixtures of cstUons of the first group 1-15
Test questions and problems 115
Ch. X. The Second Group of Cations 116
45. Characteristics of the group 116
46. The value of compounds of cations of the second group in medicine 116
1+7. The effect of a group reagent 117
48. Reactions of barium cations 118
49. Reactions of calcium cations 120
50. Analysis of a mixture of cations of the first and second groups 121
Test questions and problems 121+
Ch. II. The Third Group of Cations 124
51. Characteristics of the group 125
52. The value of compounds of the third group of cations in medicine 126
53. The effect of a group reagent 126
54. Reactions of aluminum cations 130
Card 6/10

Chemical Qualitative Semimicroanalysis SOV/4288
55. Reactions of chromium cations 132
56. Reactions of trivalent iron cations 135
57. Reactions of divalent, iron cations 137
58. Reactions of manganese cations 139
59. Reactions of zinc cations 141
60. Analysis of a mixture of cations of the third group 143
Test questions and problems 145
Ch. XII. The Fourth Group of Cations 148
61. Characteristics of the group 148
62. Tbevalue of compounds of cations of the fourth group in medicine 149
63. The effect of a group reagent 152
64. Reactions of silver cations 153
65. Reactions of lead cations 155
66. Reactions of monovalent mercury cations 157
67. Reactions of copper cations 159
68. Reactions of bismuth cations 161
69. Analysis of a mixture of cations of the fourth group 162
Test questions and problems 164
Card 7/10

Chemical Qualitative Semimicron-lysis SOV/4288
Ch. XIII. The Fifth Group of Cations 166
70. Characteristics of the group 166
71. The value of compounds of cations of the fifth group in medicine 167
72. The effect of a group reagent 168
73. Reactions of ions formed by arsenic 169
74. Reactions of antimony ions 174
75. Reactions of tin cations 176
76, Reactions of divalent mercury cations 179
77. Reactions of mixtures of cations of the fifth group 180
Test questions and problems 185
78. Analysis of mixtures of cations of the first, second, third, fourth
,
.
and fifth groups 185
79. Analytical classification of ions 191
Ch. XIV. The First Group of Anions 192
80. Characteristics of the group 192
81. The value of acids containing ions of the first group in medicine 193
82. Reactions of SOZ anions 195
83. Reactions of SO anions 196
.3
Card 8110

Chemical Qualitative Semi-icroanal:rsis SOV/4288
84. Reactions of GO, anions 198
85. Reactions of P094 anions 200
86. Reactions of PCI--- or B 0`2 201
2 4 7
87. Reactions of C 0- anions 202
2 Z
88. Analysis of mixtures of anions of the first group 203
Ch. IV. The Second Group of Anions 205
89. Characteristics of the group 205
90. The value of acids containing anions of the second groups in medicine 206
91. Reactions of Cl-anions 207
92. Reactions of Bf-anions 208
93. Reactions of I- anions 209
94. Reactions of 97' anions 210
95. Analysis of mixtures of anions of the second group 211
Ch. XVI . The Third Group of Anions 212
96. Characteristics of the group 212
97. The value of acids containing anions of the third group in medicine 213
Card 9/ 10

Chemical Qualitative Semimicroanalysis S07/4298
98. Reactions of N03 aniona 213
99. Reactions of NO~ anions 215
100. Reactions of CH 39OCr anions 216
101. Analysis of mixtures of anions of the second group 217
Ch. XVII. Analysis of a Chemical Compound (Salt) 218
102. Preliminary observations and preparing the substance for analysis 218
103. The detection of cations 219
101+. The detection of anions 220
Appendixes
1. Solubility products and solubilities (mol/liter) of some slightly
soluble substances at 250C 222
2. Dissociation constants for some electrolytes at 18-250 223
3. Description of a cabinet-type test tube rack and its approximate
dimensions 225
AVAILABLE: Library of Congress
Card 10/10 JA/rn/sfm
10-5-60

the method of dettriTtinihon on em,. a.,;
vctume and Lh, Cof.
C',efficient, of swell
C-1
Is
ir -VLr wtv! it,
the 1~-.t fi" are t "
T. n.

T ILE) V. K.
Tile, V. K. - "The Problem of Ylethod-, of Determining the Degree of
Swelling of Gels (Comparative Investigation of Vol-ametric and Gravirentric
Methods of Determining the Degree of Swelling)." Moscow State Pedagogical Inst
imeni V. 1. Lenin. Moscow, 1956 (Dissertation Vor the Degree of Candidate in
Chemical Sciences). -
So: KnizLm~aa Letopis', No. 10, 1956, pp 116-127

atlyevich; I , Vera KarlOvna; STUKOVIIIIi)
,ILF
GARBUZOV, AndroY Ign L.L.',--tekhn. red.
JI.D. , red.; T3zwvA Ie semimicroanalYBiBI Kolichestyen-
(Chemical quantitativ z. Moskvay Gos.izd-vO
n7j khimicheskii POlumikroanali (M-IPA 17%1)
"V.ysshaia shkola)" 1963. 145 P-

TILEA, D.
Basic principles in the development of the engineer's brake valve. p. 601o
REVISTA CAIIDR FERATE. (Caile Ferate Romine) Bucurestis Ramanias
Vol. 6, no. 11j, Nov. 1958.
Monthly List of East European Accessions (MI) IG, Vol. 8, no. 7j July 1959
Uncl.

TTIIII, D.
-1 )i-Inciples for project! rr- autonati(~
CAII02 (FillCUr(23ti, 'rOl. 1, ~7c-~ t,. 1" 7
. - ;, .1.
30: ol Bast 7, "o.

TILMOMOV, B.; LOSS', G.; XAMIN. N.: SHABALIN, S.
In this photography sections of the Union of Sows Reporters. Soy.foto
20 no.10:1#4 0160. (KM 13: 10)
1. Predeedatell pravlenlya f otoeektoli Soyuza shurmlistev Kasakhokoy SSH
(for Tiloksistov). 2. Pr*daed&tell pravlenlya fotosektall Soynsa zhurnalint
Istonskoy SSR (for Loss'). 3. Predesdatell pravlenlya fotosektsii
Altayak"o otdolentya Soyaxa shurnalistoy SSSR (for Zmlinin).
4. Potokorrespondebt gazety "Orlovskiy kossomolets* (for Shaballn).
(Photography, Journalistic)

- TILENEIGIG.- I-. -
Parks are favorite recreation spots for Muscovites. Gjor.khoz.Mosk. 37
no.10:41-43 0 163. (HIRA 17: 2)
1. Zamestitoll nachallnika ot(lela l,lzllturnc-proqvatiUAlnoy raboty
Upravlonlya kulittiry Ispolnitellnogo k(,f.,Afata M-)skovskogo gorodskogo
goveta deputatov trudyashellikhsya.

RU-,-'-~NIA / Physical Che-aistry. Surface Phonomena. B-13
~Idsorption. Chro4atography. Ion L-f-change.
Abs Jour: Ref Mur-Y-himiya, No 2, 1959, 405c~
Author ---~~hi ~S.
Inst :Not -,iven.
Title :Specific Surface Mcasuro&ents.
Orig Pub: Rev Chim, 9, No 5, 239-246 (1956) (in Rumanian
with summiaries in German, English, Fr,~nch, and
Russian).
Abstract: ~'L review article with a bibliogre..)iiy listing 23
titles.
Card 1/1

-F

4

Adsorption and se
RM. C 305-1 M.-Th
lt
1h
E
Y

d
sed, and
Mes an
the dynamits of adsorption are
W. .
special attention is given to the work of Dubinln (C.A. 46,
0379c; 47. 2012h). Frnetionating destirption, such as the

of PhCH,Cl at 0, 5. 10, 15, and 17* by a turbulent
ciorptio
d
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ar
ous
roca
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scusse
.
nar a
r stream
Or Jam
y
fractioas which have been adsorbed together My De dF-
3orbed in this manner. In the case of technical hydrocarbon
Mixts. from. e.g., petroleum gases, the desorption occurs at
-125*. Gas chromatography is just a
higher temps., 115
eciarized case of such a process. T
sp ech. equipment Is
shown In which such selin. can be run on a large scale; the,
rocess Is economical. - Werner Jacobso!!...

L

d nVerfies of the monacrystalling Rillra
1
n ji
4d. -96., CLILUxanch).
engh RuElp
170 r
0

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SIO
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.
p
der contill flon until table rels appearrd the
t 11 tolol vo~ fur 24-48 tirs. (tt.
sit natiln quid, d te'd, the

tile get clit into tile desited piles. pff]
212A red),
by C and iii the same vessel, then washed with
=
,
or I (the latter for tnknsparent products),' ;j
at 2 S. Wi 0 va r, and ed below 60% z2ve S':
bard silica gel with a, morctryit. mtcrohomogene= strue-
' DO. I",
ture. Its satn. capacity for IftO. EtOlf, and U14 Wag AOOL4
23.
517g higher than that of the usiml cow. products, unit %* -r
!
Ill GurfltCle At 450-4W sq,rn./g. It bad a gr&Lt Affittity for
0- cad Oil- and a marked pleachroism. Adiscoutinulty.
r
's
lir
i l
with T
i
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d
l
d
l
I i
rrwa v%
a
on
sot
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ytj=
iorpt
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c a
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(j
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-

A liew iolor ved~04 sit
C4 Fe vTRF"O=-C-
it' lid C14'. &Udii rtreflars flAiffl. 3, a) 3/4, *-102(1052)
4, b 110 In aq, 501n. ij F, e chu.. !!-, I bN11,011.11CI in fie
r nee of 114, then 1,12804 6 added until tile P11 b 63.
W
, so , ascomt
1 In will react with C111% in the dis%olved or t:.
state with formaliwl ot a blue color, wiiieb can be n-wit Iwil,
for detection and detti, of CjIf3; it Is fairly stablL. which db-
tingialshes it from the tinic-horiorcd lloi a reagent (Ber.

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TILENSCHI,.Silviu
The structure of liquids and liquid surfaces. Rov chimie
7 no. 1: 615-623 162.
I.. laboratory of Colloid Chemistry, Bucharest University.

i13--' A p pp, -, t,, !;
.- -41u~~y
-4-
Wei
POM -
Ttmm nmstm~

DUDAS, Jozsef, okl.olajmernok;_TILESCH, Lt2jpklbanYamernok
A new evaluation of the Lovaszi-series of the Lovaszi oil field
from the view point nf oil-geology aM exploitation. Bany lap
94 no.5034-347 Ky 161.
1. Koolajlpari Troszt, Laboratorium i Foosztaly, Budapest.

-TIUZCII Diane
IntrcAucing tie ii-Ar-matinriftl subscriter's dialing -in ,hc
I j
Hu-igurian taic-x network. Hir Lechn 15 no.9:280-284 " 164.
1. Central Telegraph Mice of the Hungarian Fost, Bu~!apest,

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ACC NRt AP6031395 SOURCE CODE: UIV_011V6TIb5~160~1000210006
AU'rHORS: Ris, V. F. (Doctor of technical sciences); Dan, G. El. (Candidare of
echnical sciences)l Shershneval A. No (Candidate of technical scionces); Tilevich,
A. (Engineer)
T-ORG, none
TITLE: Some work of the Nevskiy Machine Building Works in studying the flow part of
centr:Lfugal compressor machines
SOURCE: Energomasliinostroyeriiye,, no. 9, 1966, 2-6
TOPIC TAGS: centrifugal compressor, multistage compressor, exhaust diffuser, gas
c;ynamicaj compressor rotor
ABSTRACT: The results from studies of the flow parts of centrifugal compressor
machines are given. The effect of intake chambers at various periods of timewere
sLudied. Tests of a final stage with a pump-type rotor vith a short bladeless
diffuser and a symmetric pear-shaped helix made in the presence of an intake chamber
and with axial intake gave practically identical results (see Fig. 1). The effect
of certain rotor parameters is studied on the basis of an earlier work of V. F. Ris
(Tsentrobezhnyye kompressornyye mashiny. Izd. Mashinostroyeniye, 1964). It is found
that when the exit angle (~2 is increased from 15 to 909 the efficiency of the final
oc: 621.515.ool.

ACC NR,
Fig. 1. Effect of intake chamb6r or,
characteristics of various0stages:
I and II - N - 20 and 45 :
0 - stage with axial intake;
I.- stage with intake chamber
OJL-I
4a, 4~ 411
43
stage increases at first, and then decreases, When tho relative width of the rotor
b2/D2 is reduc3d to 0.0131, the maximum values of efficiency are reduced by only 1%
(see F~g. 2). The effect of bladed-diffuser geometry is also studied.
A?6031395

ACCISIR, AP603i395--'----'

-In

11L Q!~ Q;
Orig. art. hast 11 graphs, 2 tables, and formulas.
SUB CODE: 13/
A4
w 0
cli 04 in
0
0
in
ho
0
43 4-)
(D
4) 0
4-4 r-i c\j (NJ
0
0 OS
0
4- -g CV 1 0%
Q X M
'S 10
4-, 0 '~~
r~ 0) UN
c~ .0 W 4 0
rq cu c\j rn
4-) \0
U)
b0 0) 11
ri
rT4 :x0 cm %A
SUBM DAM none/ ORIG REF: 002/
OTH REF: 001
Card

'_062012-6_T_-__EWT(1 fp(M)IDW(M) P(
AP603lP97 SOUAWC CODEt "UR e1'1F4_'/iW01010F_ n000d1_2_f6_0f_6
AUTHOR: TLlevichp 1. A. (Engineer)
ORG: none
TITLEz Aerodynamic forces acting on centrifugal compressor diffuser
vanes and losses in vaned diffusers
~ ~p
SOURCf: EnbrgomashLnostroyeniye, no. 9, 1966, 12-16
TOPIC TAGS: centrifugal compressor, compressor, diffuser design,
qompressor performance ) 0qce0,)L1A)1qmie_ f-oRcc
ABSTRACT: The performance of a centrifugal compressor can be changed
by adjustiag ten diffuser vanes. However, such an adjustment can only
be made after compressor shutdown. In connection with designing a
mechanism for diffuser vane adjustment while the compressor is in opera
tion, an experimental investigation was made of the aerodynamic forces
a.1ting on -diffuser vanes in a centrifugal compressor. Tested was a two
age compressor model 305 mm in diameter aq peripheral speed of
0 m/oec. Aerodynamic forces were determined from static pressurn
asurements along the vane contour. The attained results show that
aerodynamL-- forces and moments acting on the diffuser vanes of centrLf-
ugal compressor can be of considerable magnitude and must be considered
1/2 UDC: 621.515.533.6.001.5

KC NR, AP6031397
in calculatLng vane fastenings. The numerical results can be used in
calculating a diffuser vane adjusting mechanism. Orig. art. has:
4 figures, 2 tablest and 7 formulas.
SUB CODE:13.20 UBM DATE: none/ ORIG REP: 004/

L 38435-66 EWP(m)/EWT(1)/W(k)/EWP(k)/T-'C'/L-elP(v)--~--Ijp(c) 04/W
AC7M. . AP6019730 SOURCE CODE: UR/0096/66/000/007/PO33/0036
AUTHOR: Dan, G. It. (Engineer); Tilevicb, I. As (Engineer)
ORG: Nevskiy Machine Building Plant im. V. I. Lenin (Nevskiy
mashinostroitellnyy zavod)
TITLE: Gas dynamic characteristics of vene-type diffusers of
centrifugal compressors
SOURCE: Teploenergetika, no. 7, 1966, 33-36
TOPIC TAGS: diffuser design, centrifugal compressor, gas dynamics
ABSTRACT: The work of a diffuser Is conveniently evaluated from the
value of the loss coefficient 9 . which represents that part of the
kinetic energy in front of the diffuser q which is lost during the
passage of the stream through the vanes, ?Md from the value of the
recovety- coefficient A j which characterizes that part of the kinetic
energy which is transformed into static pressurer
where q3 is the mean velocity bead in front of the diffuser;(5 r is the
loss of total bead in the diffuser;A 'A is the change in the static
Card 1/2 uDc: 621.5i.62I.L3.o6ool.

ACC NRI AP6019730
heat .in the diffuser, Experiments were carried out in an
experimental unit which is illustrated in the article. A table gives
the characteristic dimensions of the apparatus. Based on the
experimental data, -graphs show the effect of the number of vanes on
the characteristics of the diffuser and the effect of the diffuser
channel, The following formula is derived
8= 0.23 (2q/I)3 - 0,00204 + 0, Is
I )(!/-1 -0,002
@,-me
where A is the density of the grid; CK is the abscissa of the mean
curvature of the middle line;O( 4-1~~ is the angle of rotation of the
shape in the grid, degrees. The io ula is said '-o be valid for values
0
of 0-~ 4 7P 400* Orige art* bas: 5 figures and 2 tables, [061
UB CODE: 21/ SUBM DATE: none/ ORIG REP: 001
Cwd

YErIMOV, Aleksey Nikolayevich; PARYHUTA, AndreT Nikitovich; T=VZ9#
Israilt Alskeandrovich, TULK lazarl Stalevich; YALODBLYUM#
'-Bd~is Borisoviclif '89POSIDUKOV, Xselyan Grigorlyevich, ZAKHAROV,
D.Ha, lnthener-podpolkovnik, red.; HYASHIKOVA, T.Y., ;akhnered.
[Principles of the theory of airplane flight) 09novy teorii poleta
samolets. Moskva, Voen.izd-vo M-va obor. SM. 1957. 443 P.
(Airplanes--Aerodynairics) (KIU 11:5)
If
FWE I BOOK EXPLOITATION 341
Yefimav, Aleksey Nikolayevich, Parkbuta, Andrey Nikitovich, Tilevich, lzraill
.Aleksandravich, Tuler, IALzart Brulevich, Felldblym, Bori_s_B_o_r1-s8Wc__h,
ana SUAYOshnikov, Kaslyan Grigorlyevich
Osnovy teorii poleta samoleta (principles of the Theory of Aircratt Flight)
MOsc0wj VoYen. izd-vo Min-va obor. sm, 1957. 43 P. No. of copies
printed not given.
Ed.: Zakharoy, D. M., Fingineer-Col.; Tech. Ed.: "nikom, T. F.
PURPOSE: This book is intended as an aviation and technical text book on the
secondary school level, It W also be used as a textbook in the study
Of the fundment&ls Of gircr9ft flight theory for the flying and tech-
nical personnel of the Air Forces and of the All-union Voluntary
Society for the Promotion of the Army., Aviation and Navy. The intro-
duction is intended for readers vho embark for the first time upon the
study of the fundment&U Of aviation. The text is approved as a text-
book for military avlation and technical schools by the Chief of the vuz
Administration of the Military Air Force.
Card 1/17

Principles of the Theory (Cont.)
341
COVERAGE: The authors discuss the fundamentals of applied general and high-speed
aerodynamics, the fundamentals of the aerodynamics of propellers, air-
craft performance,- stability, control, maneuvering flig4t. The book
oontains 4 tables and 360 figures. There &-re 29 Soviet references, 4 of
vhich are translations.
TABLE OF
CONTMITS:
Introduction
Initial Information on Flying Machines
3
3
Basic Parts of an Aircraft and Their Purpose 1.1
SECTION I. BASIC INFOM4ATION ON AERODYNAMICS
Ch. I Basic Properties of the Air 24
1. Subject of aerodynamics 24
2. Basic 6sracteristic a of the sit (pressure., temperatures, density) 24
Card 2/17

Principles of the Theory (cont.)
34!
3. Basic physical properties of the air (inertness, viscosity,
compressibility) 27
4. Structure of the atmosphere and variation of the air parameters
py T, and 30
5- Internatio al standsxd atmosphere (MSA) 33
Ch. II Bas -ic Laws of Aerodynamics
1. Preliminary information
2. Equation of continuity
3. Bernoulli Is equatiox
4. Principle of velocity measurement
36
36
38
41
47
Ch. III Visible Pattern of Air Flow 51
1. Resistance of the air to the forward motion of bodies 51
2. Principle of reversibility in aerodynamics. Wind tunnels 51
3. Air flow pattern 53
4. Basic parts of a flow pattern 53
5. Air flow pattern of various body forms 57
Card 3/17

Principles of the Theory (Cont.)
341
Ch. IV Aerodynamic Forces 62
1. Principles of formation of overall aerodynamic force 62
2. Factors &ffecting the overall aerodynamic force 64
3. Formula for the overall aerodynamic force 67
Ch. V Aerodynamics of the Wing 69
1. Geometrical characteristics of the wing 69
2. Geometrical and aerodynamic twist of the wing 74
3. Angle of attack of the wing 74
4. Pressure distribution along the wing profile 76
5. Total aerodynamic force on the wing 81
6. Displacement of the center of pressure along the chord with vary-
ing angle of attack 82
Components of the total aerodynamic force U
Lift force of the wing 8
9. Profile drag of the wing 92
10. Induced drag of the wing 94
11. Total drag of the wing 99
12. Relationship between aerodynamic forces and their coefficients 101
Card 4/17

Principles of the Theory,(COnt-)
341
13. Aerodynamic quality of a wing (lift drag ratio) 1022
14. Order of determining the aerodynamic characteristics of a wing in
wind tunnels 104
15- Polar curve of the.wing 106
16. Parabola of induced drag 108
17. Wing high-lift devices (flaps, spoilers, etc.) 109
Ch. VI Aerodynamics of an Aircraft 117
1. Lift force and total drag of an aircraft 1-17
2. Mutual interaction (interference) of the parts of an aircraft U8
3. Aerodynamic quality of an aircraft (lift drag ratio) 320
4. Polar curve of an aircraft 120
5- Incidence angle of a wing 123
6. Methods of reducing the parasite drag of an aircraft 123
SECTION 11. AERODYNAMICS OF HIGH SPEEDS
Ch. VII Initial Information on Aerodynamics of High Speeds 130
1. Basic equations of high-speed aerodynamics 130
Card 5/17

Principles of the Theory (Cant.) 341
2. Speed of sound 134
3. The Mach number 140
4. Stagnation temperature 143
Stagnation pressure 146
9.0 Variation of the parameters of air p, T, and with increasing
speed 150
7. Obtaining supersonic flow 153
8. Propagation of weak disturbances 156
9. Boundary waves of weak disturbances 159
10. Shock waves i6o
Ch. VIII Wing Aerodynamics at High-speed Flight 166
1. Critical Mach number 166
Subsonic flow about a wing 172
3. Mixed flow in the presence of local shock waves 174
4. Mixed flow in the presence of local and bow shock waves 180
5. Supersonic flow about a body 184
6. Wave drag of wing 185
7. Effect of compressibility of aerodynamic characteristics of a
straight wing 183
card 6/17

Principles of the Theory (Cont.)
341
8. Use of velocity profiles 193
9. Special features of the aerodynamicsof a swept-back wing 194
10. Special features of the acrodynamicsof a wing of small aspect ratio 200
Ch. IX Aerodynamic Forms of a High-speed Aircraft 202
1. Critical Mach number of an aircraft 202
2. Increasing the Mer of an aircraft 2o4
3. Aerodynamic arrangement of the aircraft components 205
SECTION III. INITIAL INFORMATION REGARDING AERODYNAMICS OF PROPELLERS
Ch. X Characteristics of Propellers 210
1. Purpose and principle of action of a propeller 21-0
2. Basic parts of a propeller 212
3. Geometrical characteristics of a propeller 211
4. Kinematic characteristics of a propeller 215
5. Classification of propellers 216
6. Angle of attack of the blade element of a propeller 217
Card 7/17

Principles of the Theory (Cont.)
341
7. Angle of attack of the blade element as a function of the flight
velocity, the number of revolutions, and the angle of incidence of
the bled 219
Ch. XI Aerodynanics Forces an a Propeller 222
1. Aerodynamic forces acting on the blade element of a propeller 222
2. Aerodynamic forces acting on the entire propeller 223
3. Thrust of propeller 224
4. Useful power of propeller 227
5. Paver required for rotation of propeller 229
6. Efficiency of propeller 230
7. Operation of a fixed-pitch propeller in various flight conditions 231
Ch. XII Principle of Operation of the Variable-pitch Propeller (VI$h) 235
1. Principle of operation of variable-pitch propellers 235
2. Comparison of the characteristics of fixed-pitch and variable-
pitch propellers 239
3. Advantages of variable-pitch propeller 241
4. Practical use of propellers 243
card 8/17

Principles of the Theor7 (Cbnt.) 341
SECTION IV. STEADY MOTION OF AN AIRCRAFT
Ch. XIII Relationship Between Forces Acting on the Aircraft and the
Characteristics of Its Motion 244
1. The Airplane's axis sys~as 244
2. Equations of motion of an aircraft 245
3. Steady and unsteady notion of an aircraft 248
4. Forward motion of an aircraft 249
Ch. XIV Horizontal Flight of an Aircraft 251
1. Definition of horizontal flight on an aircraft 251
2. Diagramof forces acting on an aircraft in horizontal flight 251
3. Conditions for achieving horizontal flight 252
4. Speed required for horizontal flight 253
5. Thrust required for ho;rlzontal flight 254
6. Curve of required thrust 2-56
7. Curve of required thrust with consideration of compressibility 257
8. Curve of availd-ble thrust 258
9. Method of thrusts of N.Ye. Zhukovskly 262
C ard 9h7

Principles of the Theory (Cont.)
4. Characteristic ve'locities of horizontal fligbt
11. Range of velocity
12.. Excess thriait
13. Two conditions of horizontal flight
14. Factors affecting the characteristics of horizontal flight
Ch. XV. Climb of an Aircraft
1. Definition of climb
2. Diagram of fori:es which act on an aircraft in climb
3. Conditions for achieving climb
4. Speed required for climb
5. Thrust required for climb of an aircraft
6. Angle of climb
7. Vertical take-off velocity
8. Ceiling of an aircraft
9. Climb speed of an aircraft
10. Effect of wind on the climb of an aircraft
341
263
266
266
267
269
280
280
281
281
282
283
284
285
288
289
290
Card 10/ 17

Principles of the Theory (Conto)
341
Ch. XVI Gliding of an Aircraft 291
1. Definition of gliding 291
2. Diagram of forces acting on an aircraft in gliding 292
3.' Conditions for achieving gliding 292
4. Speed required for gliding 293
5. Gliding angle 294
6. Two gliding conditions 295
T. Range of gliding 296
Ch. XVII Range and Endurance of rUght
299
1. Definition and foximula, of flight endurance 299
2. Fuel consumption per hour 300
3. Mazlin endurance In horizontal flight 301
4. Definition and formula of f3lght range 302
5. Fuel consumption per km 303
6. Nazin%rup 0
T. Effect or wind on flight range 307
Card U/IT

Principles of the Theory (ront.) 341
SEMON V. E=LtBRjUf4, sTABILTTy, AnD COWML OF Alf AIFWLANE
Ch. XVIII Position of Center of Gravity (CG) of an Airplane 310
1. Center of gravity of an airplane 310
.2, Mean aerodynmic chord of a ving 310
3. Position of center of gravity of an airplane 313
4. Correction of C 0 longitudinal position(longitudine.1 shift of the C G) 314
Ch. XIX EquilibrImm xt an Airplane 31T
1. Cqnception of equilibrium of an airplane 317
2. Longitudinal equillbrims of an airplane 318
3. Transverse equilibrium of an airplane 320
4. Directional e(plIbr1ma of an airplane 321
5. Lateral equilibrim of an airplane 323
Ch. XX Stability of an Airplane 325
1. Concept of stability of an airplane 325
2. Longitudinal stability of an airplane 328
Card 12/17

Principles of the Theory (Conte)
341
3. Aerodynmic center of the wing and of the airplane 329
4. Con4ition for longitudinal stability of a ving alone 331
5. Condition for longitudinal stability of an airplane 332
6. Graphs Mz : f(CO 335
7. Basic factors effecting the longitudinal stability of an airplane 339
8. Directional stability of on airplane 343
9. Transverse stability or an airplane 346
10. Transverse stability of an airplane at large angles of attack 351
11. Lateral stability of an airplane 353
Ch. XXI Controllability. of an Airplane. 356
1. Concept of controllability of an airplane 356
2. Principle of operation of the rudder and ailerons 356
3. Methods of reducing forces on controls of an airplane 357
4. Longitudinal control of an airplane 364
5. Balancing curves 366
6. Longitudinal control. In curvilinear flight 3TO
7. Basic factors affecting the longitudinal control af an airplane 3T1
Card 13/17

Principles of the Theory (Conto)
341
8. Directional control of an airplane 374
9. Transverse control of an airplane 377
10. Transverse control of an airplane at large angles of attack 379
11. Methods of improving trwverse control at larp angles of attack 380
12. Relationship between transverse and directional control of an
airplane' 383
Ch. XXII Stability and Control of an Airplane at High Speeds 384
1. Effect of the compressibil-tty of the air on the stability with
respect to load factor 384
2. Effect of the c%.jv asibility of the air on the stability with
respect to speed 385
3. Effect of the compressibility of the air on thp control-eurface
effectiveness 387
4. Effect of the cpressibility of the air on the hinge nuoment 389
5. Aileron rev roal 389
6. Violent banking of airplane at higb flight speeds (forced banking) 392
Card 14/17

Princiylea of the Theory (Conte)
341
7. On the relationship between trawmrse and directional control-
lability in flight at high Mach nudbers (inverse banking reaction
when pedal in pubed forward) 394
8. On limiting spod 395
SBCTION VI. UNSTEADr MOTION OF AN AIRCRAIT
Ch. MaII Ac~celermtlng, Decelerating,, DITUwpi and Plare-out of an Aircraft 397
1. Accelerating'of an aircraft 397
2. Declerating of an aircraft 398
3. Diving of an aircraft 399
4. Irlare-out of an aircraft 399
Ch. XXIV Take-off of an Aircraft
1. Stages of norml take-off 400
2. Take-off run of an aircraft 4W
Take-off of an aircraft (separation from ground) W2
Leveling off of an aircraft 403
C ard 15/17

Principles of the Theory (Cont.)
341
5. Factors affecting the length of-the take-off run 404
6. Take-off distance
7. Saae special features of none-vheel airplanes vith regard to take-off 407
Ch. XXV Landing of an Aircraft 409
1. Stages of norml main 409
2. Gliding of an aircraft In landing
3. Leveling of an aircraft 410
4. Flareout 410
5. Ground contact of aircraft 411
6. Landing run of an aircraft 412
7. Factors affecting the length of the landing run 412
B. Landing distance 413
9. Scme special features of nose-vbeel airplanes with regard to
landing 414
Ch. XXVI Steady Turn or an AIrplane 415
1. Definition of steady turn
415
Card 16A7