SCIENTIFIC ABSTRACT OVSYANNIKOV, B. M. - OVSYANNIKOV, M. I.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001238620016-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: June 21, 2000
• Sequence Number: 16
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

77
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110"d*vp 34TO-9, volotilov ma 6repailD VVI, 349
meta Ile: Ineft st ivis,
MAWft
MWO 4' 196): 47- 1' 477
i~6G ~.'Iliuthore away&*. miethOte, of astal *moil* tests at the boil-
-of 214aid hyd"gone -the speolm" were cooled and deformd in a
"diflid "A Improved Dewar lowk-Amooraturo vessele fte ~ tests were carried
olat'41 *~MIUPWMODO P-5. (R-5) tosting machine at a 49formation rate of
educes
It It roooinsended to.ses cylindric" 0i'afts as this r
ape
~the.orvov Affignitidsee :?be matura of Ahe,stressed state arising during the
Aerokiaticift of' the, speciame Gan ~b;o established &Go' orUM to the angular
Atstri~%Mob ~ of mi"Osis I in'~ vlomlski' Us' very: m1betmatial effect of ban&~I
part
,.7ii44t Aow., total error ~Udst~rni"34:Lth* IMW*h&"G" oh"&Gt*r-.
Istio's `V* -Able, m.thod. anovats to or, the matima stress. . Based on a
stat4atloal..anslysis-it'vas fowA that-reliablio romiltware obtained with
Ahis Sethod'A"o,th for'britum."CAnotile listalso -:Thor* a" figures and
`-7

ACCESSION KRt AT4001248
furnaceswith seals to ensure hermeticity of the system at relatively
large displacements of the clamps of the testing machine, heating
elements for the furnace. and control circuitry. Some operating
features of the furnace* are discussed. Orig. art. has: 15 figures.
ASSOCIATION: TsentralIny*y nauchno-iseledovatellskiy institut
chernoy metalurgli (Cmtral Scientific Research Xnatitute of Ferrous
Metallurgy)
SUBMITTEDo 00 DATE ACQ# l0Dec63 ENCLt 02
SUB CODZs AP# MA 50 REF SOVi 006 OTHERs 000
COM 2/4

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ift ~-Vithlll Stainless steal Plat" at tbe, qpsnup
&a vltk'MS12 bfttIM 010-
The tomparetwe on as test piece vas measured w1lb a 'by
~1000ter. rm lGed Vag applied to the test piece after It v"
Aid, Alle'It, me belid at
AsodDe. "Tows am ame rigives.
-1taitnatim amdoo-balsimatelleMy lostitut ebernoy
Instits" or Pwrois nL44W
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ACCESSION NR: AT5003403 S/2776/64/000/038/0115/0118

I&beCe_v. D. V.; Solotilbv.-B. V Ouvannikov
I I M. Te
wlnw~_ I
v
lendh t sting ejutpwnt jor verl lov tggaratures
r

SOURCE., Moscow. Teentrailnyy nauchno-LadledovattVifty lastitlut thernoy metal-
~'lurxli~ Sbornik tvudov, no. 38, 1964. Wovyye,m4tody ispytanly setallovj 1."t
iograficheakiye issl*dovantya I makhenichoskiye Ispytaniya metallov (Now m6od
-:In the analyses of metalafmatallosiraphic investigatioag -and mechanical analyses
,

J
;of -metals
), 115-118
L

-Z
ne low tamp-
101AM te He testing,'cryostat,'liquid helium, liquid nitroge
OP

[~~era
ture test

RAM.- The development of solid state physics re uLres an ever-increasing
a of methods suitable for low temperature.testing, and particularly unidir-

'
tatic tensile tests. The authors' Institute has-been vorking on the
ectional a
simplification of available tensile testing machines, An Improved design'vas also
sought Vith.a view to reducing the amouat of Be used so a coolant. Furtherwrtj
the new machine was to have a capacity for testing single crystals, polyerystal
11m microsamples. mid studard.cyl1ndrical specimens 4 to 5 M in diameter 'Or

f
2

0
vi'&ov VLIB found.to be most conve.
-4
several mo e 8
.Cryostat suggests V IL
~
1
~~?"40:1'&ndccmpsct." ;LOON.Of beat'Abrough.its walls. was"diminimbed by tightening

b, -air. pis'is~'":tho -:leakage. of the tool
~-ihs comecti6he ta
a use, of ru b
b 41ditional Cooling i th liq-
&at - Isolati, i a' improved - y Vi
on from 'the siub on a r v a
The loads applied werei.reciorded by means of an d#ctl2ography SYS-
-utd tiftrogen.
,
too. A centering device.provided reliable centering of the work pieces The

working cidamber'was isolated with mirror'fi ishe 0.1 mm thick,*
n d copper sheets
clad with Cr, A or Ag. However, the search for better equipment continues.

-OrI&I ta:bsit _3 figures. p
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chernoy metaillurXii,
nyy nauchno-isel4idovatel skly-fastIM
ASSOMMONt Tsontral P
','Moscow (Central ferrous metallurgy scientific research institti
to)

SURIMMI 00 ENCLI BUD CODIJ 59, NH
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"t nppllcxtlon~af -tontactleas ku power circuits) furnace
*ve.1
Mal Ir
oppen atid
t trol zetbod -during -je
empera urs, icon _ji. 2 and stress i~upturs strength tests
W. _TS intra I nyy nauchlb'- ssledqvatel ilkly'lustitut chernoy metal-
il.41MCIft x0ac'O
8 oridktivat metal-
ant
lografirbeski" 'Assledovani-ya
ye nikhanicbeskiye lspytaniya metallov.(New methods.
I d anical anal
a2s; metallgaragbic Investlitat L'onivan mech
_.,qna_ yses of met yees
iv
-t.viitals~ :119-122
~T turatlo~n AA6". ~Ontactlisis ra Me ontrelt furnace tempera-
amps c
rAture regulationy:,ereep test, 'itreas rupture stranStb test, tester
-Th thors investigated the possibility of introducing a more advanced:.'.
a Au
contactleas wbieb
method:,of temperature control by means of a saturation eboke
would anable,the use of a centralized remote control system, eliminate substantial
rheostat heat emission Into the working area, and-facilitate mintenance* In
earlier paperej thedesign a of saturation cbokeB as a means of In-
nd employment
LCarj 11

2776
'ATS
'duci1ve coupling, -between the primary circuits of furnace beating elements and the
control, ciieuits had been discussed. - The iron saturation choke has an &C. coil j
on tWouter cores and a D,C. excitation coil an the center core. The magnetic
flot.p4smes only through 'the outer cores. The A.C. voltage is not induced by the!
excit0tion'coil. The furnace beating range lies between 300 and 800 C and the
**I tage In 0 for the Initial 300 C and 25 v for the maximum temperature. The
choke capacity'is fully employed byconnecting the choke to the primry circuit
of the beating elements through an autotransformer vhose transformation factor is
equal to .2.- Both are connected individually to each of the three sections of the,
furnace to provide accurate temperature control along the height of the working
area.-: Light and sound signals Indicate irregularities in the control system.
The proposed system enhances the reliability of a test installation, cuts the cost
of electric power and secures a more convenient and saf or operation of the control
pantLq~~ Origo~arto.basi I fij*re~
ASSOCIVIONt ?sontrall-nyy-na -L' skiy Ustitut cbernoy metal lurst I,' -
uchno asledovatell
terrotif-metallutd scientific research Institute)
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ACCIESST01 NF: Ar4013114 S/()032/64/030/00;1/022P/0220
',T'TYCP,: Nsynrnikov, B. V.; Lebedev, D. V.; Yelekhinq A. %; Vollnov, V. F.
TITLE i An instnllntion for testing lonr range durability, imder voscuum at tempera-
furns lip to lFWC
SMRCE: Znvodskaya Ipborptoriya, v. 30, no. 2, 1964, 228-)29
TOTTC TAGS: dur-bility, durability test, lonp, rpnge durRb'Llity, vocilum effect,
+erperrture effect, vacuum oven, heated vncuura oven
ABSTRACT: The install.-tion consisted of a two-section steel vnclzum oven of cylin-
drical shape, 29 em in diameter and '40 cm long, provided with P weter ~F-cket and two
centrPlly locnted rpdiation heaters. By these means it was possible to brine the
temperature ur to 13MG within. 20 minutes and to 1800C within 65 irdnutes. Powever,
It wAs found thpt a too rrpid rise of terperature caused an accelernted evolution of
gases from the test samples placed in the oven, which affected the vacuum. A
gradual step-by-step rise in tempermture ves found to be the proper procedure. An
additional source of error in a vacuum of fluctuating magnitude was due to the
prosenco of eoualtz-tlon loads of the leverage system of the testing mechire.
71 gure 1 on the Fnelowures gives the structural details of the vacuum oven,,_njM;Ps
4,

L 3M3_65 Zv?(d)/W(ji)/OdP(w)/UP(c)/EWA(d)/EWP( 11P
AccmioN WR, Ap5w7680 WP(b)/EWT(1)/FdA(C) Pf_4
JDIWIEM
Andriano,,~t Tu. Ye.; LebedevI.D. V.; Oveyannikov, B. U.
V
-TITLEs A Method.for strain in
testij small specimens at a temperature UP to 1600C
vi-
C89~~-, avodslc4a laboratori"t "V- 31* M*
.3o_1965 3674369
Sotal defornationg vacuump
16111"Le Astio defomtion/ IFX 0*2 mchine~
~"ABMCT .j - Atecbniquo of strain testing x1crospeeizens wider vaouvin (or in inert
'9" --temperature up-to %= is- describedo- -The Method MPIOY8 the 12E2-_2-7~
M0+010CMI t&&+4vijw AgriA its Aeopribed by V, P. Kano-, ieWco'and ~ DO XF
-Vinoaradov
r; fte baiff Mch
-11001 0-400) 0- -600,
load',cavaoitv 1000 kgj direct loading; acale divisions 0 600, 0
w4--0,4000' kgj~ zwdx= -tQwPer 6-ture -1 1 - YPPPMM pressure,
1 X 1074 ~M LTg,' dC?fDr=-
06r ns 45:1:
-test tWoraturo--2-li!6volti),---The-RAchinO Pormith
L t imm
era. Figure i6surt gives the definitiaa
-measuring several- stre Na ~ - 7ri ~_. * 11 cn. the %o:
ze of- disen ..The-optiml size Of a -test
-or th '-variabl __q
a as-- describing ifter si ajo. -epe
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orate rboomendations- are nadi for Bjpec ication of
-;--speciam di4"iozw_, AM oon if
cdhtrdi.a~d afteurement during Ibe testing. lemato inaicate that the
Wt. are-in oo4lete acodrd with tlhe~: at Avotim outince pro-
in 66ST I Orige art. hast 3 figues.
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ACC NRs AP6010101
(d),,~WI(W)/EWP(t) IJP(c) Mj"
SOURCE CODE: UR/0129/66/ooo/6-6ii6o6~-/-O-'0-65
AUTHOR; Lebedev, D. V.; Maslenkov, S. B.; Ovoyannikov, D. X.
ORG: TsN1IChERMET
TITLE: Mechanical properties of E1827 alloy at low temperatures
SOURCE: Metallovedenlye I termicheskaya obrabotka metallov, no. 3, 1966, 64-65
TOPIC TAGS: nickel alloy, chromium containing alloy, tugsten containing alloy,
molybdenum containing alloy, aluminum containing alloy, alloy property, low tempera-
ture property / E1827 alloy 10
ABSTRACT: The tensile and yield behavior of E1827 nickel alloy (0.03%C, 9.85% Cr,
5Z W, 5.652 MD. 4.352 Al) at 20C to -253C has been investigated. The alloy wape
annealed at 1170C for 6 hr and water quenched. It was found that the strength ~u
clar-acteristics Increase linearly with decreag ing temperature. At room temperature
the tensile and yield strengths are 108 and 70 kg/m2; at -120C, 119 and 80 kg /mm2;
and at -253C, 140 and 82 kg/mm 2. The ductility changes Insignificantly with a drop
In temperature, the elongation remains around 47%, and the reduction of areaaround
40-442. The deformation along the gage length was uniform; no necking was observed
at any temperature tested. The yielding at temperatures as low an -253C was smooth,
and the streas-strain curve showed no serretimNas observed In some metals and alloys al
low toWeratures. At room temperature the alloy is prone to deformation aging. which
DC: 620.17:

(c)
~'i"c '.r. -,nnt~ an,i I m:xy Julormat Ion on
ZaL13.-, prnc,.;L ln %n~n riu'uons of --Lool lKhltN'la,'
-.oon%ra: ln~-j ina'..tut
Ik %
Lr rv, ~r,~Jov no. 46, 1966. 3,)(-j t 3 it, II r,~-
. .,L yc I I Gplr~vy
al 96-92
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J7% Laro wl'l dw'roa (i(Il an. 7,;,(1
c. aro pronwiLvu
1 LWan foun'j that at
cr~t,-'cal duformatior, of Lho ribbon was 16,)5~. A '~ all temporaLuros 3UL".*(J(;' a
Cord 1 /2

OVSURIKOV, B. W.
Tension test for metals. Standartizatsiia 25 no.3-46-48 Mr 161.
(KERA 14:3)
(Metals-Testing-Standa.rds) A-

OVSYANN]KnV, B.P., lr--h.
R,-3. I Its c, t-,, -' g'-laize -,r.*- - - 3. . -,, .
I sel n , . I . : " ,, a ',,- . Iw - R -, ". , -
1. r'hplya~.,, rsk !:( nstit-jt mikhnn,- tai sl,, i 7 :e~ - - %, ~: i ,
3e! '3k(,,,,) 0 ~.q! va.

SERGEYEV, M.P., prof.; OVSYANNIKOV, B.P., Inzh.
Determining the output of the choppers of silage harvesters.
Makh. I elek. sots. sellkhoz. 21 no.3:5C-51 '63. (KMA 10~: 2 /
1. Chelyabinskly inatitut mekhanizatsil I el.ektrifikatsli
sellskogo khozyaystva.
(Mowing machines) (Ensilage)

SOV/88 58 W 6/7
AUTHOR- &Mgg&LL2Lk_~p Candidate of Technical Scienneo, ind Kivirr), O.J.,
Candidate of Technical Sciences
Exhaust Nozzle of a Piston Engine With the Addition of Atmoepherl'~
Air (Vykhlopnoy reaktivnyy patrubak porshnevogo dvigatelya s
prisoyedineniyem atmosfernogo vozdukha)
PERIODICAL: Trudy Moskovskogo aviatsionnogo instituta, 1958, Nr 97; AddAtion of
a Supplementary Volume in Jet Apparatus (Prisoyedlnenly-~ dopol-ritr-11noy
maasy v struynykh apparatakh) pp 181-190 (USSR)
ABSTRACT: The authors consider the problem of using the kineti7 energy of exhaust
gases for the addition of atmospheric air. They dpscribe the teat
installation used in their research, give sow- numprIca.1 data and
several graphs illustrating their findings. The main probl~-ms of
their research vere: 1. to determine vhether the insta.1lation of an
a] nter on jet nozzles of aircraft piston engines leadB to a natice-
able thrust increase in spite of the high frequency of thpir -yelps
(600-1200 cycles/mInute); 2. to determ:Lne the influence :.f thp pres-
sure of the supercharger an the thrust of the combinpd. 1,-* The
authors arrived at the folloving conclusions: 1. The addition of
atmospheric air to jet exhaust gases by means; of an open ej(-&0r
Card 1/2

IMASE I BOOK EXPLOITATION SOV142~0
Ovays.nnikov, Boris Viktorov-ich
Teoriya i raschet nasosov zhidkostnykh raketaykh dwignteley (Theory and Dl-siF~3
of Pumps for Liquid Fuel Rocket Engines) Moscow, Oborongiz, 196o. )46 p.
Errat-a slip inserted. 10,000 copies printed.
Ed.: I. L. Yanovskiy, Engineer; Managing Ed.: S. D. Krasillnikov, Engineer;
Ed. of Publishing House: S. I. Vinogradakikh; 71ech. Ed.: V. P. Rozhin.
PURPOSE: This is a textbook for students of aeronautical and machine -bt.Li I ding
institutions of higher education specializing in the theory and design of
pumps for liquid fuel rocket engines. The book may also be used as a manual
for engineers and technicians interested in pump systems for aircraft power
plants.
COVERAGE: The book is based on a synopsis of courses given by the author and
on Soviet and other literatuiv. It discusses the theory and design of pumps
for liquid rocket engines, as well as characteristics and fuel requirementg of
such pumps. The author emphasizes that he has made ample use of the Soviet
T'neor-f and Design of Fumps for Liqlild Fuel kCont.. ) SOV/4230
experience in pump building presented in a book by Professor A. A. Lomakin,
Doctor of T~?chnjc&j Sciences. The author thanks Professor V. 1. Polikovskiy,
Doctor of Te~~hnicaj Scienres, for his comments and suggestions con,'erning ths.
manuscript. There are 2t, references: 23 Sn,.,Jet, 2 English, and I Germam.
TABLE OF CONTKN~,S:
Foreword
Ch. I. :n t roduc, t i on 7
1. Area of application or pumps in liquid fuel rocket engines
2. ReqlLtrements of pumps for liquid fuel rocket engines 11
3. Classification of pumps 17
Ch. ILI. Basic Concepts on a Centrifu~l Pump for Liquid Fuel
Rocket Engines 21
1- Arrangement of centrifugal pumps -, 1
2. P--er and efficiency of a pump 4
5. Flow of liquid through the rotor of a rentrifugal pump
4. FUndaMent-al equation of turbopumps
5- Expressing Pump Preesure through cir.-u-lat1(,n 14 T
6. Equa*.Ion of energy with resWet to motion 44
Card 21 5

OVSYANNIKOV, 11.7.
Relatlonshl;7 betwear. thp Impe' '-Pr pro-smi-re of a radial
bladed machine anrl th.- mownt ~f inertia f-r--s.
Izv. vys. ucheb. zav., av. tpKh. F 't- I .
'?U~A ', ~
( I',- boma - h ! ne e - F 1 u-' I I YnRni~ - 9 ,

/_,j Y,'Y Al
ID ~? SUV~3848
a. vju& EXPLOITATION SOV 11-M-97
Moscow. Aviatslonnyy Institut Imeni Sergo Ordzhonikidze
Prisoyedineniye dopolnitellnoy massy v struynykh apparatakh;
sbornik statey (Mass-Flow Augmentation in Jet Engi.en-
Collection of Articles) Moscow Oborongiz, llj,,r'. 230 P.
(Series: Its: Trudy, vyp. 9fi Errafn -Iip inserted.
2,21C copies printed.
Ed. (Title pavp)* Kvasnikov, Professor; Ed. (Inalde
bool,'. S.G. Boshenyatov (Deceased); Managing Ed.:
S. Zaymovskaya, Engineer; Ed. of P1,blishing House:
T":A. Valedinskaya; Tech. Ed.: L.A. L2bedeva.
PURPOSE: This collection of articles is intended for scientific
workers at engineering schocls and research Institutes and also
for engineers -ci,;1-ing in experimental design offices.
CCVERAGE: This collection contains abridgua U'1jsL:rt___ns from
the Department of Aviation Engine Theory, Faculty No. 2, of
the Moskovskiy aviatsionnyy institut (Moscow Aviation Institlite)
Card 1/12

Mass-Flow Augmentaticn in Jet Engines (Cont.) SOV/3848
the mixin,7 chamber and permit the calculation of the length
and the profile of the mixing-chamber wall, as well as the
effect of the ejection coefficient and the turbulence factor
on the mixing. It was found that the length of the Initial
sections of the mixing chamber depends primarily on the
ejection coefficientlk and the magnitude of the test con-
stant(X which characterize the structure of the turbulent
flow of the driving gas. The length of the mixing chamber
is essentially Independent of the difference in the velocities
and temperature of the flows. The profile of the wall of
the entrance section is extremely close to a straight line,
slightly inclined with respect to the ejector axis. This
angle of inclination depends primarily on~k , 0( , the velo-
city ratio u2/ul, and the temperature ratio T2/Tl. The
compressibility of the basic flow has a negligible effect
on the mixing process up to sonic velocity. The analytical
results are supported by experiments with an air ejector.
As an incidental result of the study it was shown that, for
a mass flow of the basic jet equal to C-5 kg/sec and a pres-
sure ratio of 1.85, an Increase in thrust equal to 25-35
percent of the thrust of the basic jet could be obtained.
Card 3/12

Mass-Flow Augmentation in Jet Engines (Cont.) SOV/3848
geometry of the walls without taking Into consideration
dissipation forces (viscosity and themoconductivity).
Comparison of the analytical results with experimental
data shows that the properties of the complex flow ob-
tained by the aforementioned theoretical treatment coin-
cide with the properties of the actual flow observed in
the ejector; that Is, the character of turbulent mixing
In an ejector is the same as in a free turbulent submer-
ged jet. The flow in an ejector may thus be regarded as
a flow of a submerged jet which is deformed due to the
presence of the engine walls whose effect may be theore-
tically identified with the effect of a system of point
vortices where the turbulent-viscosity coefficient is
assumed constant in determining the vortex Intensity.
The actual velocity fields inside and outside the engine
differ from the Wal, particularly near the walls, be-
cause of the-presence of the boundaz7 layer. Corrections
for the effect of the boundary layer are given which
permit determination of the actual velocities Inside the
engine. The thrust determined from the analytical equa-
tions was found to be in good agreement with experimental
C ird 5/'12

t Erginen (Crnt. R OV, `3 3 4
Kudrin, 0.1., Candidate uf Technical Sciences. Pulsating Jet
Nozzle with Mass-Flow Augmentation 98
I. Theoretical Investigation 99
1. Calculation of the thrust cf a sli,ple pulsaL..L*1,j,_,
jet nozzle
2. Ener6y losses associated with the process of
exhaust reaction ic.,4
3. General estimate of the efficiency of a pulsating
jet nozzle with addition of atmospheric air IC7
4. Possible processes in a compound jet nozzle 121
5. Calculation of the process with gradual inflow
of supplementary mass 125
0 Calculation of the process with expulsion of supple-
mentary mass 139
II. Experimental Investigation 144
1. Test setup with pulsating combustion chamber 144
2. Test setup with a single-cycle combustion chamber 17C
3. TLSt setup with a one-cylinder piston engine 178
4. Conclua-lons from the experimental investigation 178
Card 7/12

Mass-Flow Augmentation in Jet En6lnco (Ccnt.) SW3046
This paper presents a theoretical and experimental study
of the offects of addinp r.c i- __ )Li3_*L;ii,j, jeLo.
It ir ~:!. ., ._ ,tie addition of atmcspheric air to a
pula.iting gas jet may lead to a considerable increase
in its impulse. The addition of supplementar:j air mass
is not only due to ejection, that is, the parallel addi-
tion of air Into the driving jet which is associaLed with
mixing, but also to the Interaction of separate masses
of air added gradually. Two forms of this gradual addi-
tion are possible, namely gradual expulsion of additional
mass and gradual Inflow of air behind the driving jet.
The largest increment in thrust (up to 12C percent of the
thrust of a single nozzle) was obtained in a compound jet
nozzle with an open shroud which includes the three basic
forms of the process of mass addition (eJection, expulsion,
and graduAl infl--w of -Ir behind the dr1,.,ir- jr~t). The
gratlual Inflow is the basic process which p~oducee a large
increment in thrust and determines the character of Its
variation as a function of the basic parameters of the
pulsating flow. The thrust Increases obtained in the pro-
cess with gradual inflow were found to be close to the
curr(,qnonding calculated values based on the assumption
of no losses :!i_ie to friction or vortex formation. This
Card 8/12

--SOURCIE CODE:
ACC NR, %P,-)036862 - - -- UR/O147/66/6C,-/,-
AUTHOR: Ovsyannikov, B. V.; Borov~;Aly, B. I.
ORG: none
T ?:,oticm of enerc,,y '.rans c::, In cent.r.fugal and r-xu
by c1rcula*.1on and Coriolis orcus
SOURCE: 1VUZ. Aviatsonnaya '.eKhr--r'.a, no-4,1966,107-113
TOPIC TAGS: centrifugal PUMP, T1XCd f-low PUMP, Pump per'or..ance
analysis, pump design 7 '^0,0Z / 0 /- / zFoL, cE
ABSTRACT: An analys-s is presen~e,~ of some problems of
cent.rlfugal and mixed-flow pu-mps the point of view o"' energy
transl~er processes. It was prev-'ously shown (Ovsyannikov, V.,
Avlat31onnaya tekhnika, no.2.,i963) that in a centrifu~,L! t~,c
ener,,y Is tran3A'ered to the fluid by Coriolis inertia Corco.-
circulation forces (i.e., forces associated with the c.'rc-.-*-o,-, of
relative velocities around Impeller blades). Formulas are erlvei~ loor
calculating these forces, and relationships are obtained ~"nese
lorces anci certain geometric pump parameters. It is note.~ ... a Z; t- I s
Lype of approach to pump analysis makes It possible to exp.ar. various
Card 1/2 UDC: 621.67

ACC NRj AP6035952 SOURCE CODE: IIR/0129/66/000/OiG/0040/0041-
AU'n1ORi Babakov, A. A.; Lebedev, D. V.; Ovoyannikov, R. M.; Ol'yanin, Ye. A.
ORG: T_%NIICkERXU
TITLE: Mechanical properties of Khl4Gl4N3T steel at -253C
SOURCE: Metallovedeniye i termicheskaya obrabotka metallo-i, no. 10, 1966, 40-41
77,c r,~;,Ie 60-eej,,A_~
TOPIC TAGS: chromium manganese nickel steel,'boron containing steel, steel property.
steel subzero temperature property/Khl4GN3T steel, Kh14G14113TR steel
ABSTRACT: The properties of Khl4Gl4N3T and Khl4Gl4N3TR steels in the as-cast and in
hot-rolled conditions have been investigated at -253C. Annealed at 1050C and water
quenched, the steels had a fine-grained austenitic-ferriti( structure, while the
Khl8NIOT steel used for comparison had fully austenitic structure. At -253C, rolled
2
and annealed Khl4Gl4N3T steel had a tensile strength of 160 kg/mm , a yield strength
of 49 kg/mm2, and elongation of 342, and a reduction of area of 281, compared to
185 kg/=2, 68 kg/MM2, 32%, and 42% in the Khl8NlOT steel and 152 kg/=2, 58 kg/1=2,
38% and 50% for boron-bearing Khl7Gl4N3TR steel. KhlhCl4N3T steel in the as-cast
condition had a much lower strength. (70 kg/mm2) and extremely low ductility, and an
elongation and reduction of area of only 5%. At -253C, as-cast Khl4Gl4N3T steel had
a crystalline fracture which was not observed in Khl4G.14N3TR or in Khl8NlOT steel.
Card 1/2 UDC; 620.17:669.14.018.8:536.48

OVSYLT'ITY'Ov, B.V., 1-nnd.t#4khn.nauk
Inflow of rne into a :ylirlmr wit)~ raria'la vol-.ime. 1auch.4ckI.
-rvR.Ph!7nl7', naph.1 prih. no.;': ~~71 'SP. Owl Ii" I ;. : 10 )
1. Prv1ntAvloqnn AnFil-oveHm aviatnionnym inatituton.
(Fluid dynamics)

OTSTAINIKOV, BeV.; CHEBAMSKIT, V.F.
BeeUts of testing high-spead centrifugal puspe. 1&y. vjvv. achob.
say.; av. tekh. ne.W04-111 158. (KMA 11:6)
1. NDskovskiy aviatsiowW Institut, Kafedra AD-2.
(Gentriftgal pumps--Testing)

OVSTAIIIIIKOVA B.V., kand.takhn.sank
ConcerniV, MA.Bater's article piblishf-d la "Inergonashin-
strnanin" No.4, IqS7. under the title "Conforml method for
specifyiW, blade profiles for Francis-type turbomchinery";
letter to the editor. Xnargnmashinnstroonle 4 no.5:15 R7 '58.
(Hydraulic turbines) (14IRA 11-9)

OVSYANNIKOV, D., kuznnts, brigadir kollektiva komhjunisticheskog,- truda,
deputat Verkhovnogo Sovnta SSSR.
Wim achieves 6routness only in work. Sov. prof 9r Juzy 16 n( .,?i~ :
10--9 0 lb(~. (MIRA 11:11,1
1. Odpaskiy zavod iment Tanvarskogn vosetaniya.
(Odessa--VRgetable garleninj- (Irnitenriag)

009006000000000*:::90:10040 !0::10090040000000000
a --Lj- it cm AV a
a opt, a 5 ?w-;
d
0
-ts
*0-0 7ton,.-
0
"1"41 48M us sell rkww-
-All sq uuj sudied uvi-ad ju IiOmi~v mU ~nj~.j
AitAn aqj tunarmvenj aqi w slissain aqi &aqzwa tm &~Ua 400
o9 Pwq Jwtv "1"'14 NO all'Ift '(511"Alu UI UaA4) -IIn-lJ
007 smilkolvue ~%mJ twittid qspa pouppucu jw)djd pul, q1tim 040
I.q. *-amAj uO.,tosd M txm qptu aw lutm tdxa w4i 00
0z jn~j "IqnAo amimaAd K)u pqp qua ssnow %V 0 pb Lussi
::AF -lui lawnsOl" ma ajnprjjd ajiPAl UWOMAO 99 fO - 9 U roo
IjIfAI.ftMPqUbW (I;Ufk INFINUM IZI-0 On UA%Up) um &Mpnus 00
Ilu " sum mU AmAo aqi w tasgs clu peq &mop
jJ191111M -A4Iu &.11USP4 64 1"IfIRAO Iva Insain aqii-K .100
Aglaw.18"t- P-Ii-as 4MOA 10 41fun -- 0- 1 V-:1
JO Wm-*%4 KL- - = '" ml 4-7 an) ?
'1l a`OOP-'O-VZ *9"1 '"1w#7 A WPM ,Goo
.PY "9r missal AG 4,() -61 00
00- "IMPOPINt" --
06.. P"40 Ism 10MIND
00" .06= OMP Rom p mV "1 00
so- - ---- - - - - - - 600
gel... 6., - ., IV 00
4 T-T 4 -Ttwo M W-W T-T-Y-11 I 4--j I 1 0 d v v 'T v
d a 904 0 IV tim Onow ItIcifirajam a's It '4 " (I n a i 1 0 1 1 Oro
a 0 0 a 0 0 0 a wic~ewo 0 0 0 0 0 0 0 0
0 #1 IF 09 W 0000 so 0 0

OVSTAKNIIOV. 0.
i;c. ., -- '56.
. ffol,lirq,o or, rod j- . Straitell 2 no.6:1~ Je
I I rders (p 1.) 1 , : " )
(Scn4'fnldine)

AIX W-71 --- 1 i SOURCE CODE: UR /2
PM IT6=M3 63974V0()10Wv133161Yj
AUT! IOR t 60
4 4 05 'S
ORG: tam of &"its of the &b. RLwAAtj, A SsSR (institut fiti)d
asoU AN SSBR) 5
TTTLEe. Semiconductor circuit for'powering a noncommutator motor for an opicentral.
BSJLdc station
-SOURCE: AN SSSR. Institut Miki zemlio Trudy, no* 35, 1964, 133-137
.10PIC TAGS., semiconductor device. electronic circuit. electric motor, soismologle
station. sAsmologle instrument
ABSiRiM Test runs usinG a semiconductor-powored noncovmtator motor showed that
0
~..wfwn the temperature of the surrounding medium exceeds 20 C, overall PC-for consumptl
Increanst, This Increase can be reduced significantly us1ne som
by jeontluctor diodes
`(*chepitie for commutator is shown)* Origs art* hast 3 flaurese LroBt Y6 1, not
COM NCO 93 SURH DATE: none

1. OVSYASNI~OV, G. F.
2. USSSR (600)
4. Cattle Breeds
7. Work practice in improving Yaroslav cattle, Sov. zootekh, 7, No. 12, 1952.
9. Monthly List of Russian Accessions, Library of Congress, Februw7 -1953. Unclassified.

OVSTA12ITKOV, G.F., I-and.sml'Rkokhoz.nauk
InterrelatIlmnship bntwean the lAngth )f gastatio)n Finli liv-
weight of newborn calvms. Zhivotnovolstvo 21
s 959. MRA 1~1:1)
1. .4oekovslWa sml'9lcokhozvaystvf)n-itqu aluiAnnipi ',non'. K.A,
Timiry&zeva.
('01tiv-18)

OVSYANNIKOV,-G.G., aspirant; LIDIN, Dmitriy
Electronic cale,ilating machines. Avt4*., talen. i sviaz' 6
no.10t16-20 0 162. (YIP-A It,: 1,1
(Railroads--Flectronic equipment) (Flectronic computers',

OVSWiNIKCVP G.G., aspirant; LILih, Dautrly
i1lectronic computers. Avtom., telem. i eviazi 7 no.2-.18-22 F 163.
(KIRA 16-3)
(Electronic computers)

ACC N17- AT6o 2 39 j 2
its firia.L Iona the probabi 1 1 tv of m;j,,,neti, Lj,,)f- i ,j u r-
q. kit;
wnere qi(L) is ttie prot)aoi ; I L Vof a SeCtI011 I ;-A I L ki re i n t iii--, i)Z
of zones, ano w' is the probaoi',ILy Lhat Like Correcting code wi4l Correct
by repeated readouts. Algoritnais are given for recording on tape and for re,.GIiL.
Orig. art. has: 13 formulas and 2 figures.
SUB CODE: 09/ SUBM DATE: none/ ORIG REF: 006/ OTH REF: OU2

0vs'w;-.'Ix'--;' 3. V.
ASYANNIKOV, ;. V. --"Thc Histogenesis and ~.eactive ~;Langes in the Fkin
Tissue of the Ram Scrotum Follow-inr Crstrati,n under Experi-mental
conditions." Min higl,er -Iducation USST. Leningrad Veterinar,' Inst.
Leningrad, 1955. (Dissertation for the Degree of Candidate o 7f ~-iolagical
Sciences.)
SO: Knizhmya Letopial, No 5, Moscow, ~eb 1956

OVSYANNIKOVA, 1.A.
Studying X-ray apeotra of the compound IUS. izv. Sib. otd.
AS SSSR no.11:8CP-87 161. '. ',I I ""J 15 : 1
1. Iwtitut neorianIchoakoy khimil Sibirskogo otdoleniya 'Al.
:USSR, 1:0vosibirsk.
(Nickel sulfidos--Spectra)
(Spoctrum, X-ray)

SMDT, N.V.j DONTSOVp P.M.1 KRASILININOV, Z.N.; SHVACH, Ye.N.;
MUNNIM. I.I.
Heat treated carbon steel for shipbuilding. Sudostroenie 28
no.9:44-48 S 162. (MIM 15-10)
(Platea, Iron and steel-Testing) (Shipbuilding)

--QVSYAUMWV. 4pr' Yladialrovlch; SXRGNYBV, V.I., red&ttor; ZUBRILINA, Z.F..
takhnichaski,y rodaktor-."
[Growing fruits indecrej Pledovre rastentia v comnate. Moskva, Ges.
ind-vo sellkhos.lit-ry, 1957. 109 pb (MLRA 10:4)
(Prult culture) (House PlAnts)

OVSYANNIEDV, I.V.
Vher* to obtain seedlings and plants. Not. v shkole no.2195 Mr-Ap
156. (WAA 9:7)
l.Daystvitellnyy chlon Koskovskoge obshchostva ispytateley prirody.
(Forest nurseries) (Nurseries (Horticulture))

OVSYAM,A_KOV. 1&9r.'. y1adimi;qv.Ioh- VARGANOVA. A.B.. redaktor izdatelletva;
- W-.-" ~~ ~ redaktor
[Growing citrus fruits indoors) lownstnala kullture taitrusovykh.
IZd,. 4-oe, ispr. i dop. Moskya, Izd-vo Ministeretya komunallnogo
khosiaistya RSYSR. 1956. 46 p. (KLRA 10:3 )
(House plants) (Citrus fruits)

ACC NRs
EIWT (I SCTB DD
Monograph
?4
L*ffannikovIKDnetantin Aleks9yevich
Pjw&chute_junDin1fjr~m militar7-transport planet, (Pryshki a parashyutom iz voyanno-
Us-noportaWkh samoletoy) moscow., Voyenizdat, 196h. 253 P- Mus., biblio.9
copies printed.
TOPIC TAGSt parachutep air force training., tranaport siroraftj, training eqtdpment,,
ground force-training
PURPOSE AND COVERAGEt This book describes parachute parta and equipment and
regulations for rigging and handling parachutes. It also inoludes rules for
parachute jumping from military transport planes while carriring weapons anti other
equipment,, Jumping over water and from great heights* Several recommendations on
organizing and-training for parachute-descents over towns are node. This book is
recommmded an a training manual for parachutists in flyift clubs and youth
organizations of the DOBAAF,
TAME OF CONMT5 (abridged):
introduction - 3
Cho I* Ruman descent parachutei 10
Ch. Il. Parachute instruments - 55
Cwd 1/2 UDCt 358-h 0-34

OVSTANVIKOV, K.L., inzhener
New techniques and industrial methods in Moscow construction
Drojects. Mekh.stroi. 14 no.10:26-11 0 'S7. (MIRA 10:12)
1. Glavmosstroy.
(Nnscow-Building)

OVSTANNIIOV. K.L.
, - -,
Construction in the sixth block of the Novo-Poschanyt section.
Gor.khoz.Mosk. 28 no.1.2:12-15 D 154. (MLRA 8:3)
1. GlaTM Inshener Obahchostroltellnogo territoriallnogo
upravleniya No.1 Glavwsstroya.
(Moscow--Building)

OTSUMUOT, 94 - ' RAYIIM, Yevgenly Yakoylevich; ZOLOTNITSILIT,
N.M. ~raf-. doikrto tokhn.nauk. red.; KGRELOT.A. N.I., red.;
RAXOT, Solo, tokhn,red,
(Amoost reinforced concrete at the construction site] Sbornyl
sholosobston no poligonakh. Pod red. W.DoXolotnitskogoo Kooky&,
Isd-vo TfvSFS Profludet,, 1960, 327 P. (KIRA 14:4)
Mmeast concrete)

OVRANNIKOV, Karp L'vovich inzh.; BAYYEi, Yevgoniy Yakovlevict,,
kgnd tekhn. muktdeceased); KOHNIIDVA, M.I., red.
[~'oscow experiment; experimental, assembly-line, ;in(,
uniciue construction in Moscow] Moskovskil eksperiment;
eksperimenta"noe potochnoe i uni-kallnoe stroitell-
stvo v Moskve. M( skva, Profizdat, P)C5. 255 ~ .
(MIRA 0:1)
Zamestitell nachallnika Glavnogo otdeleniym po ztl-
lishchnomu i grazhdanskomu stroitellstvu v g. Moakve f
Ovsyannikov).

- ~SYKlii~ '~, .~. .1 . . I ; . I . I . . I r,-,l .
e * ,-C A.' ~, -. . ~. It *1 ~ I . I ... : , % T, 1-:' . . . I
. - . I
:~ j F :-F S ". I ~ , - " , - . . . - , , 11 r.~ , ( , I ~ .1% :. 1.. , I , I . . I
. , enizc:a I, - , ... . . . ., ... . I

ttUGIiIKCIVP Tu. P. , kand. tekh~
nauk. retsenzmt. 'A :.PYkNSKIY, 'A-7-l'- EN K
7 '1

OVSTANBIXOV. Koustantin Hatveyevich; RAVINOV. V.N., bnd.tekhn.nAuk, n3tsen-
zent; VOLPTANSKIT, L.K., inzh., red.; WGINA, B.A., tekhn. red.
[over-all mechanization In foundriael louplakenala melchanizatalia
v liteinykh tBakhakh. Pod red. L.N.Volpianakogo. koalcvs. Goa.
nauchno-takhn.izd-vo mahinostroit.lit-ry. 1960. 76 p. (Ilauchno-
populiarmaie bibliotakm rabochego-litelshchikm, vy'p.29)
(MIRA 1,4:1)
(Found rios-Equipment nnd irupplies)

OMANNIKOV, L. -
"Lenin's wtelbock.l Hauka i zhi.qnl 28 U0.9-5-7 5 161.
(141W 14:12
Moscow
-Machinery Industry)

'OCIIER~'NKO, P.; OVS,'AT,IKOV, L., okonomist
F-fficiency of t:., i,ieceworic-bonw ani- fiyn'.otm cin ri f,,r--. Sots.
trud 8 no.10ibl-64 0 '63. (~U~-.A 16:1-2)
1. Direktor sovK:,oza "Kalacheyevskiy", Vororiezhskoy oblasti (for Ku-
chertnko).

DR&UIMA, 1-Yr.; MUCHALOVA, T.I.; OVSIANNIKOV, L.F.; OPJDCHKIN, D.&
Investigat4ng the composition
of naphthalene in the presence
Koko i khia* no.3:48-50 163.
(Naphthalene)
of decalin obtained by the hWagenation
of sulfur-reeiBtant caWyats.
(MIRA 16:3)
(Hydrogenation)

OVSYANNIKOV. L. M.;BRUYNVICH. T. S.
, -, ". --
Two cases of deep blastom7cosis o! the skin. Vest. rener..
Moskva no.5:43-" Sept-Oct 1951. (CL%(L 2 1: 1)
1. Of the Department of Dermatologr (Head - Prof. L. N.
Mashkillerson), Central Skin~Vensrsological Institute
(Director -- Candidate Medical Sciences N. P. Turanov).

CNSUIWIXOV. L.H. (Moscow)
Deep intestinal lavages for various icinde of dermatoals. Vest.ven.
i dare. no.6:46 N-D IS4. (MIRA Pi-2)
(SKIN--DISEASES) (INAKATA)

o YS1,,,',4A1N1" '*/ 4, Al
OYSTAMIKOV.- L.M.
14-
Forokeratoole. Vest. won. I dorm. ac.1:45-46 J&-F 155. (XLRA 8-4)
1. Is ?Sentrallnogo koshno-vanarologicheskogo inatituta.
(SKIN--DISUSIS)

. '. K

0VSyAVyjj[0jg 4
r, A A L M i u Poll cr 1.0 R
77m Ov%yannikov, V., On a gim flo sith ji tis~,:ht
tran,twn li,j- (ij, ItIlgil:1sq, jl,ttj if,,, jj,AA 1j,
Ito V)
lalln, t(, a -1 Itfroll
_:L,2tv tit'ly Ito ~Vlmlvill ai j.-I 0,01
.(r whi r to 1l,,. n%14 to( ij~,- pqI
-mli'm 1~
Wit 21, 1 121. RMI, t, ""i"t-1

L.
A ro rie t I F- - r~ pp T- E rr - s e r te,-4 ~,), ' - - - ~ - - f, A ' ' -' r- --)nff7rf-! (-- -,-
A ro-lynar- I cs ( Q-2 " 'f--r ' '~ '; ), C-rv, -), -J '~,- * - ,' r ~,t~ t ' F - f
Vechan`cs, Acn`er-y of **SSF, vris,
"S)-r.etricall Flow of a Current Tast a W- -i-E-1 ,cr ~n !-,.,
SO t Iz-estlya A" -S~T. Ct-~elenlye Tekhnic~xskle~. ':auk, ':-. I , '
N
~71~ne Ic53, (W-3114,2, I,' .',,Iy 11-W

on Trimmes pmbtm ki 3, 1
-- generalize(I 39MRR.~Fof the Euler-Nrbouz
Doldady Akaib N:wk S&S11 (N.S.) 91, 437--460 0953).
(Rusiiian)
Let S Ix a Tricorni domain for the Sauation

hall
Tha f ii, S cons;sts, of ;ill arc K in the j-pW)r y-%o with
~bthematf entilmints kin the x-axis (al Aand.B)and tile twochwacle.-

~MdY, 1954 isties in y;50 issuinx from these endpuints, A gener.Jized
Anal solution u(x, y) of (*) 13 said to be in class P. if: (1) v
rontInIMUS in S ; (2) U-0 on X; (3) v is twite uontinuulAy
di-TtientiMile in' .5. (the part of S for which y>O) and
oisfies (0) there; (4) Owe P%ists a function v(x) it Wil. B);
Zvo that

forijbitrary v roniinuous in Rt; (5) u(x, ~~;11611vi in S-
tile Mostion

Y) ~7,

P(3)d3

Vol. 15 go.
Jan. 1"4
rbb "Mau
I ILIN&Ld i
A PL Vestflik wimm"junly, IT", no, 5, Tr-34 I
M
(1952). (RuBS5
By perturbing unifc.rm sonic Raw the author first dwi
approximate equatiorialgr @lady plane irroUtimal v*
originally obtained b-tv' th. Phys.
182-190 (1947); them. ev. 217 Pn&Y,
(Akad. Nauk SSSR Priki. Met. Meh. It, 459464 (1947);
these Rev. 9, 4761. Then he obtains appropriate forms fot
the conditions at a strong shock and shows that the same
system of partial differential equations is valid to the eme
order of accuracy in transonic rotational Ruw beHnd a
curved shock. J. H. Gkta (Havre de Praca, Md..).
1-.U--T4-t4

C
VIPS
ties -
7/39,

Lo, B

:~~Oft inearization of an soatice, In partial derivatives of the
Via I
r
,EU,

A uvtW is PMOMW fir: the or a map-linear equation In
~ewod order Into a Ilwar Ons in thO tOrm9
-portba- derivatives of the
patloa. The Mtkod.pmIts say amber of lWep*DdeDt
-or the Original eq
a the bargetwigatian or the &U not of the
vaildb2on and Alm P*ndt a
.14 -Oft UM
"w#,jcw obtained,

jan"M 340 IL"!
N. A,

:~V.)Yh"NIKUV, ~_ V
SUBJECT USSR / PHYSICS CARD 1 / 2 PA - 1627
AUTHOR OVSJLNNIKOV,L.V.
TITLE The General Solution of the Equations of the Renorma.'ization
Group.
PERIODICAL Dokl.Akad Wauk, log, faso. 6, 1112-1114 (1956)
Issued: ;2 / 1956
At first the equations of the renormalization group derived by N.N.BOGOLJUBOV
and D.VAIRKOV, Dokl.kkad.Nauk, 101, No 2 (1955) by means of the perturbation
theory are explicitly given for the GREEN'S function of quantum-electrodynamics.
The present work furnishes the general solution of this equation and its
analogy for the meson theory. At first the aforemeLtioned equation is trans-
formed. The transformed equation is then linear with respect to the required
function I (x9y,z). Next, ansatzes for the two first integrals are given. To
each solution of the transformed equation there cor2-esponds a certain function
T~y,z), so that this solution is determined implicitly from the equation
T Y X,rmfo(x,y,z)) - ~(y,z). Inversely the followir4r is true: Independent of
the f0 f the function T(y,z) the above mentioned equation determines the
function f (X,Y,Z), which satisfies the transformed equation. Thus,
9(y/X, (X,Y,z)) - 9(y,z) is the general solution for the transformed
equation. The solution obtained applies also in the case of y-0. However, in
that case the function q has a certain form the determination of which is
shown here. The most general solution of the transformed equation for the case
ymO is explicitly written downi it can also be determined from the above general

CIV'YFI N N IV,( V, L
V
SUBJECT USSR / PHYSICS CkRD I / 2 PA - 1903
AUTHOR OVSJANNIKOV,L.V.
TITLE A Now Way of Solving Equations of Hydrod namics.
PERIODICAL Dokl.Akad.Nauk, 111, faso.1, 47-49 (11)56~
Issued: 1 / 1957
The present report concerns a new particular 4solution of the equation of
adiabatic motion gf a compressible liquid: du/~t + (1/Q) 7 p --# 01 4
d(logQ)/dt + div u a 0,.d(log-P ~)/dt + I' div u - () Here 1 . u(t,x) denotes
the velocity vectorl Q Q(t,x - density; p a p(t,4) - pressure, If - the
coefficient of the adiabatic curve. The symbol d/It denotes the differenti-
ation according to time along a trajectory, i.9. along any integral curve of
the equation dk/dt
Withtl being aslumed to be a vector with the projections the
func one F a F(j), G : GQ) and the constant matrix of the third order
L - III ik 11 are found, o that Z~ G - FL is true. Here denotes the
operation V with respect to t e variables f nrthermore, the non-
singular quadratic matrix of the third order ~(t) is defined as a solution
of the equation Mp(d 2M/dt2 ) + I M 1 1 - rL - 01 here it O'denotes the matrix which
is transposed with respect to m, and IMI the absolute value of the determi-
nant of M. On these conditions the formulas:
__;V 1 -0 -4
_' '), p - (11191d') G(M-1 x) supply the exact
u (dM/dt)M 1, Q - (I/IMI)F(V x

IMBJZCT USSR/MATH ZMA TICS/Differential equations CARD 1/3 PG - 657
AUTHOR OVSJA"IKOV L,V.
TITIR A now solution of the hydrodynamic equations.
PURIODICAL Doklady Akad.Nauk 111, 47-49 (1956)
reviewed 3/1957
Lot the adiabatic motion of a compressible fluid be described by the system
d ~ 1
AV + V p - 0
log + div 'W4- 0
dt
d log P + gdiv 0.
4V--^(t01f) is the vedtor of velocityl (t,-t densityl p - p(t,t
pressurel )r- adiabatic exponent. The operations 17 and div refer to the space
d
(Styps). Tt- means differentiation with respect to the time along an
ff . y
arbitrary integral curve of dt A406

Doklady kkad.Nauk 111, 47-49 (1956) CARD 3/3 PG - 657
2 2 2 0 0
6- + t2 '1 + 3S + 1, L - (0&1 t 2 0
0 0 F, 3)
2) r - 21 G( g( 05 )l F( ?) - 1 0'- 1 'f ( -1 ) ,
2+ + t2 1 2
~2 s ds fl 6 o
(S) - exp F, 2 L 0 2 0
~f 1 4 (0 0 0
3) r - 1; G( g( 6 g, G
4) r - 01 G - coast I F( arbitrary,
0 0) +
L - (~o 0 0
0 0 0
L 0 0 0 Here g(G) is an
0 0 0
0 0 0
arbitrary function and gl(l~) its derivative.

, -- V ~, 1, J k~ / - / A C ~,ti- I ~ .
AUTHORt OVSYA"IKOV,L.V. 20-5-6/59
TITLE: Groups and Group Invariant Solutions of Differential Equations
(Gruppy i invariantno-gruppovye resheniya differentsial'nykh
urav-neniy) SSSR
PERIODICALt Doklady kkademii Nauk/11958, Vol.118, Nr-3, pp-439-442 (USSR)
APSTRAM Within the compass of the classical Lie theory the author
considers group properties of differential equations. The
given system S is written in a quasilinear form which always
can be reached by the introduction of additional unknown
functions. The sought functions uk (k-1,...,m) and the
arguments x i are explained as point coordinates
of an E n. Under certain additional assumptions the author
gives proposals for the determination of the group of S. The
following definition seems to be very useful: the solution
u . kf(x) of S is called a group invariant solution (H-solution/
if the manifold defined in the E n by the equations u -Y (X)
is the invariant manifold of a subgroup H of the fundamental
group of S. The importance of the H-solution is that it is
Card 112 determined from a system which in general Ls simpler than S.

Groups and Group Invariant Solutions of Differential Equations 20-3-6/59
The case of an intraneitive H the invariant manifolds of which
are identical with their systems of intransitivity is
considered in detail.
ASSOCUTIONaMoscow Physical-Technical Institute (Mosko,,ekiy fiziko-tekh-
nicheskiy inst1tut)
PRZSZNTIDt By K.L.Lavrentyav, Academioian, 24 December 1957
SUBMITTIDt 24 December 1957
IVAILLBLEt Library of Congress
Card 212

16(l)
AUT*;IuR: Ovayannikov, L.V. V, I'', 7_
TITLE: Group Properties of the Non-Linoar Equation of "Pat -onij,_jr,r~
(Gruppovyye svoystva uravnenlya nelineynoy tep1.,)Tr-iA-ic:-'
PE.-IIODICAL: Doklady Akademii nauk
A713T:tACTi The equation of heat conduction
~js
(f(u)
~x R
is replaced by the quasi-linear system
,1) W . f,u)u w u
k x I x . t
(see CRef 1-7) , and it is required that thp Qq,iati-ns are
invariant under the first co-.tinuati,::!. of the
operator I
x + +
ct u W
If invariance is fulfilled, then (1) admits the oppratcr
The following result of classifi:ation is obtained : 1. 'Pcr
arbitrary f(u) the equation of heat conduction a(lmlts onli
Card 1/3

Group Properties of the Non-'.inear Equation of ,6.1
Heat Conduction
invariant solutions of rank 1 are riven.
There are 3 references, 2 of which are !',oviet, and 1 Ncr~-~viar..
A33UCIATION: Moskovekiy fiziko-tekhnicheakiy institut (moscow
Technical Institute)
1 R --: ":-"N T --'D iDecember 27,1958, by Y.A. Lavrentlyev, Acadr-mician
.;UBI.:ITTED: December 27, 1958
Card3/3

LID4TIT. Viktor Borisovich; OVSTAIIhIKOV, Lev Vasillyeviehl TULAYKOV,
Anatoliy Iiikolayevich; SHABOIN, Mikhail Ivanovich. Prinimall
uctwetiye: AMIAMOV, A.A.; BOOM. I.A.; YEVGRAPOV, N.A.; ZTKOV.
A.A.; "(ABIGOV, V.I.; LARIMOVA, Kh.Kh.; KUMYAVTSLV. L.D.:
KMASOV, A.D.; SHURA-BURA, N.H.; SUCHEGLOV. K.P. SOIA)lJKOV,
V.A., red.; KRYUCHKOVA, V.N., tekdw.red.
(Problems in elementary matiiemticsj Zadfichl po alementarnol
mntem tike. Koskvo, Goe.izd-vo fiziko-matem.lit-ry, 1960. 463 p.
(MIjtA 14: 1)
(Kathemstice-Problema. exercises, otc.)

OVSiAhwauvP L. V. (Novusiblrak)
"The Group Fropertlea Qf 6omo Differazitia.L LquaLluns IL Pactimilco."
report presented at the Prat Ali-Uif-on Ccn6reaa on Theoretical and Apilled
Mechanics, Moscow, 2:7 Jan - -,. Feb 1,,6~

OVSIANNIKOVS L.V. (Novosibirsk)
Group characteristics of S.A. Chaplygin's eq U ' FIwTF
-, 3-0 160. "a"IL 14:7)
noJt126~14 Differential equations, Linear) (A
Muid dynamicsF

OVSTANNIZOV. L.V.
Remark on the calculation of the trace of a nonnegative, entirely
continuous, operator. Sib. mat. zhur. 1 no.2:242-247 JI-Ag 160.
(MIRA 13:12)
(operators (Mathematics))

OVbYILNNI!WV, L. V. Doc PhysoMmtn ~~ci -- "Group properties of differ-entiRl
equAtiona." NoTosibirsk, 1961 (Aand Sci U6SR. Siberian Depm rtment.. Join*
Academic Council for Phys-Math anl T-ch Sci ). (KL, 4-61, 182)
-3-

:;,/0,,,,1 1 '19o,
Group prop-rtips of tha el,intion
R( w) A f t -r a t ranS I t i in ! o n~ ',,i ra, t - r i s v
dw w
L 9
j 0-
Since . however thp bo!inlary vaitip r h- ~oi
in the gpne ra I case r- -~a i n non- 1 1 n(~ q r I or t ti~ o vp -,,-)T.: nw
difficulties some ia,~thors use ,tr. nTprox , ma . .-) n f tht. '? 'I r
by simpler approximalion equations i,. nown i,, ~ ro x [Tin ~ni Pi
criticized ty U~e a .,~jr i iv r g ri
The greater the t ran:; f orma, i ~)n m i t h,
e qua ' 1 u n I h " bo I ! - - - q , , - - ; i- -, * -,n 10. 7
~~Rlculation Procogs of T"o f '. 'I- I-
Z Z Z
ly x Y
wherim A. arc- f,~nrt ,)na T,~ ~ n r , q ss
- a r d 2

6 1 /OOC'/O - C)/'("
-104
Group properties of the equation ... C111YC222
CIPISS (1.0) , K ('5) . I
0 6-2
y0 2S)
class (I1,0), K,(F) = l'(Y 29).
0
class
cla3s 11,q) E PI,I'(s), 6' -Ts
0 P., 7
To t);e class (I q) th(,re Papecially belong-s the function V (6'
it is proved that every admissible haplyrifi !,in:! Ill-.
with one of the functions (5) or can be obtained fr,m
functions with the aid of the group transformatiDn (4).
in f-:!--ti;.n9 w~.irh
investigates admissil-lo 'hnplvi- -.jr p IF:---

OVSYANNIXOV, L. V.
"Application of the theory of Lie groups to some partial
differential equations"
report submitted at the Intl Conf of Mathematics, Stockholm, Sweden,
15-22 Aug 62

LIDSKTY , Viktor lhorisoviche.44aANLIKCV, Lev asil'yevich; ITLAYMA
Anatol'-; ~,`yr)Iaycvich;'SiiAbLq;II' , Pikhail Ivanovicl-.; iX*F-VA,
A.F., rer,.; ?-,7,,,.,~I,K(,VA, tokhn. red.
(Problems in ele-zentary math~--malicsl Zadiic~.i pc elenentarnei
Yo.1v-, Fi=--i,t~-1z,

GUcYANTJIKOV,-L.V.,,doktor fiz.-natem. nauk; ZELENYAk, T.I., Pand.
RZ.-matem. na~ik
Savlet-Am-rican s -mposium of rrathematicianE In Novosibirsk.
Vent. AN SSSR 33 no.1101-06 N 163. (MIRA 271j)

01100YAliNIKOV, L.V. Olllovosl',lirr~.)
"Invariant grou-, solutionn. o' the muatlons of hydi-Odynaiics"
Roport pre sc!nted at t:... .'nd A I-l-Uni on Conj-.ress on 7r.~-or - , i c-i I -int' ,- i : ir-,d
Mochanicv, Moscow 2-) J-ir. - 1, Fel.) L4.

OVSYA%- - 7, 1 . '.
L , 'lt~ -,it f- " .- 1-1, - - - I
r. ~- . ~,.. 0 -1 ,, 0
; I ".
I . ; '- - cl -.' 1 ,
bw o f- T-t ~ , ; , , ) ~ -, t - t N . . . : .
. I . .!;* i ~ -1
~ I - :~,Al. .
C., - ..-k 1F , -,,
i- . - - -,, t AN " ~ .. 1, ; 0 '

"'j Vi,
S, all
1.~Orlthly Lis'~ .,Us.

OVSYANNIK('V, M. ; GIIIJDAKOV, 1.
New books. Grazhd.av. 20 no.4119 Ap '63. ()URA lb: ~')
(Bibliography--Aeronautics, Coanercial)

OVSIANNIKOV, M.A.
Method for the rapid determination of work fun..-ticn. -rady Slt,.
tekh.i.nst. no.2-4:53-56 159. 14 3'
(Surfuce energy)

OVSYANNIKOV,, Mikhail Gerasimovich; VORONOV, P.Ye., inzh., retsenzent;
- - bbVGOPOL, V.I., insh., retsenzent; DUGIRA, NA.0 tokhn. red.
(The organizing power of technological progreas'jOrganizuiu-
shchaia aila tekhnicheekogo progressa. MDskva, Mashgiz, 1961.
109 P. (BibUoteka mashinostrottelia. Seriia: Peredovala tekh-
nika oanova kommunisticheakogo truda, no.1) (MIRA 16:1)
(Sverdlovsk-Machinery industry-Technologic&l innovationL)
(Sverdlovsk-Comanist Party of the Soviet Union-Party work)

OVSTAKNIKOV, N.G., partorg.
Mighty arsenal of socialist industry; twentieth anniversary of the Ural
Plant of Heavy ftehinery Construction. Test. mah. 33 no.7:94-97 JI 153.
(K6RA 6:8 )
1. T&ntrallnyy koultot Kommunistichemkoy Pw*tii Sovetskogo Soyusa na
Uralmshisavode. (Machinery industry)

OVSrANNIKOV, M.I.
MW
Lwwdiate and late results of tonsilleetcs7 in rheumatic fever. Vrach
delo no.10:131 0 160. (MIRA 13:11)
1. Klinika ukha. gorla, nosa (zav. - dotsent Ya.D.Kissionzhnik)
Zaporozhskogo Instituta u3overshenstvovanlya vrachey.
(TONSM--SURGERY)
(RHEMTIC MER)

OVSYAMIIKUV. 11. 1.
.qpa. Veat.otorin. 20
Bronchonnonh",osl!o" vith fired for,
NIRA 12:11)
no.2:111-112 14r-Ap '58.
1. Ix kliniki bolezney ikhu, gorla t nosa (tav. - dote. Ya.D.
Niosion2hnik) ZaporozhRknio inatitiita isover9henstvovaniyft
vrachey.
(IMOlICII03COPY,appar. & inatritmpnts
bronchcosopha(roucapn with filred rminleR (Aus))
OCSOPUGOSCOPY, appar & inntniments
same)

OVSYANNIKOV, M.I.
Pathohistological characteristics of inflammatory and reCencrative
prodesnes following radical Burgay-1 with biological tamponade or,
the ear of animals. Zhur. uah., nos. i gorl. bol. 21 no.2:24-27
Mr-Ap '61. (MIRA 14:6)
1. Iz otarinolaringologicheskoy kliniki (zav. - doktor med.nauk
V.O.Kalina) i kafedry patologicheskoy anatomii (zav. prof. I.I.
Madvedev) ZaporozhBkogo instituta uBovershen8tvo-~aniya, vrachey.
(EAB--SUHGZKY) (MUSCLES-TRANSP 1A NTAT ION)

ZVEREN, A.F,, in7.h.-. KAJI.-ALAPOV, inzh.; MAMR, ZJI., insh.;
CFV,;YA0IKDV, M.!,_ inzh.; SEUL~CA, Ms.. inz? .
(,oneerninL the uve of a glass fitwr tape in the manufacture of'
cables. Vest.elextroixom- 33 no.6:61.-62 Je 16,1' . (MIIfj~ I I , I
(Electric cables)

OVSUNIIIKOVJI M.I.
Simplified auditory probe. Zhur. uah., nos. i gorl. bol. 20
no.'6s87 V-D 160. (kd'(A 1512)
1. Otorinolaringologicheskoy kliniki (zav. - dotsent Ya.D. Missionzhnik)
Zaporoxhakogo instituta usovershenstvcrvaniya vrache
(MMICAL INSThUNENTS AND APFAttATUS) (&AR71ii )

OVSYAN-KOV, M.J., Cand. Medic. 6cl. (dice) "91oloc-71cal i,Aci
for smadica-I Operations am~ A-~-Llc-antrotomy with Facklr.,-- ~lFlc-
tic," Dnepropetrovsk, 1)c,1, 16 .:.)p. (Dnepropetrovak Med. Inat.'
(KL Supp 12- 1, '28?).