A FR: IZVESTIYA VUZ AVIATSIONNAYA TO: IVUZ AVIATSIONNAYA

• Document Type: CREST
• Collection: Consolidated Translations
• Document Number (FOIA) /ESDN (CREST): CIA-RDP91-00772R000100110022-1
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 89
• Document Creation Date: December 29, 2016
• Sequence Number: 22
• Publication Date: December 31, 1983
• Content Type: ABSTRACTS

Determining the Basic Parmwters of an Air-
craft Whose Flight Peth Includes a Low-
Altitude Flight Phase, by S. Yu. Skripnich-
anko.
RUSSIANr perl Izvestiya VUZ Aviatsionnaya
Teklinika, No 3, 1967, pp 110-116.
o,
Jan 69 374,193

IwIation 8atween Woij.,ht ke.,;istunca and Cost
Or a No-Stage lioeirecuvoriA)lc oiliace I.,.ocket,
by A. A. Kuziietsuv, lu pp.
Rll$S1A,Ii,v Pers IVUL, bor Aviat Tekh Vol lu,
No 4. 190, pli 9-15.
Ait'.1/RSIC/1'r-088~s-0
Sci/Spaoe
Pyr 69
377,419

Stability of 'Am-Dimnidonal boundary-
Layer Flow of an Inemqtressible Pluid
In the Case of Small Accelerations,
by N. Ii. 1-fildtin, 13 PP--
per,, Vuz Izv. Avints. Tekh.,
11
Vol 10., 1 o It., 1967v ?p
Dept of Hwa APLOUTJ T-2154
sci/p a 3689935
Oct (Y

Effilct of Plm Bomdarim cn the Aerodynavic
Characberistics of a Ming att a Ncrwtaticnary
Mbvmmnt,, by Z. M. Nugmmcov. 5 pp.
XMIMp per, Izvwtiva VUL Avi&Wcmaya
T*hnika,, No 4-,-M-I, pp Mi--29.
FM c
468-69
aw 69 388,565

On the Problem of the
Control of Elastic
T. K. Sirazetdinov.
Synthesis of Optimal
Flying Devices, by
RUSSIMAO per, Isvestiys VUZ Aviatsionnaya
TwIhniks, No 4, 1967, pp 30-40.
PTO - S -.3" c, / - '!~- ~
Feb 69 375,,398

illvwti(,Iaticn of the kffnct of i)ischarp of
uxil:U-iij iAr QAw6,,, into ti'm
Clwkrm~ma un wo (kxi 'luLbiteb :17.e~uju (Avaritticnp
by ye. 4. I;U.J(XIoiov. 15
IMSIAio L)er,, lzwstiya %Nwiiikh Ud-k--vnykh
Zavedali . Mi~atsi(~maya TigN;M-a. .;o 4,, 1964j,
pp 69-7&
ivr 69 '177.017

,iu.- 4~?cus.Wility of Sbrulatijiq Cavitation
Amww uvta in '~tx;tim) (Xvitriftujal Puipi; cki
by 11, ~;# 'Ar.illuve ij PP*
14Zsle7,HO ~jer,, lR2!tjja Vys3hikJl udy-.iAlyjxll
Mm- qmiv. Avik-tsicrui&a Tlaaklmika, LJO 1,r 1967,,
A, 470
sciAuduvi c?ji,,,r
j Lblu 69 382l985

%w Questim of 1;)qxu3.pmta.L Invastigatim of
3140mcnic quxbina Cas by
V. U. Pivitilovidi. 8 pi).
IU;SIA4j, per# IZ%Wtiya WS1 I UQ-,a!FA
ZaVWJML , Aviatsicmkwa Tpldmika# No 4. 1967,,
7.
AlIVE-TUA-M-24-240-68
sci/j.)rq)ulsicn and fuels
apr 69 377t918

'IixnlcL) of Frrors in l:'.'Lckj
A Ul I
tcv-l:uv,.! ai U-m, i;iw~r6~tjwc of ,itcci Oviracb-3r-
jithY; (TUD) g, hil
"Mil mg'lp 11110ve
1,~Lukiinikai Jo 4, 1-9671 124-129.
sci/ !.aoPULic1l ~U--I;
c-.Ct 69 3950323

CON.Oftucting the Supersonic Part of a
Nogglo hY GIVOU Velocity Distribution,
by V. M. Posin.
RUSUAN, per Izvestiz VUZ Aviats Tekh,
No 4.0 1967, ;P 130-136.
('?(I
Mar 69 378,616

Doternul,nation of tho Nalawni Qscillatinf-,
Procluoncien Of 3helld of C,=,)Iox "U'apo
llith Preo TAgess by G. 71. Salnikov,
A. G. ',"Oenukov.
:WSSIAlt, por, Izvestiya llysshild-l
'
11
'abobnY101 ~',aveConij; AOLatelonn
,Ito I
I 101 ':0 4p 19M m 143-1113.
TUVI TIT F-11,719
Sel/ 01,0 369.,121
oct 68

On the Hquation of Relative Weights of an
Aircraft, by N. A. Fouin..
RUSSIAN, per, Izvestza VUZ Avintsionnaya
Tekhmika, No 4, 1967, pp 149-IS4.
Alk7PTD7MT-24-348-68
Sic-Aero
Apr 69 380$335

*Wlawnsm and w4fJoJj&3 Gravitation,
tr Tat M. shapime
MWIANO Fws 1 11 Udnbzaft
angwx ft"Saff"Al - EM SM u
Vol Wo Ila Its * X95"Mmf
Wu TT F"U.X?
SCKL
Dft 60 371olU

ila-goar-di cn Orinbusdai in rlim, I-YV Akr. Tzilantov.
16 ove
L'ort lzw:;!ktx ~4.3udlikli UdxAil ki
ZawdaAji, AviatsiMaya 'Udl-&Ka, 140*,.1-1967#
AL, IBA4,~fi.6-24-209-61j
,j - L, ~
CA
"y 69 3810121

Invastigation of Flow Interaitim Dulng the
Injoctin of a Gew into the Si"ruadc Secticn,
by D. S. vimgradav.
XMIAN, per# Izv, AM Aviai*amaya T*lv~,
No 40? 1967, pp 94-99.
FM-ID-SpecicC 297-70
oct 70

A ,:)'tudy of the iWehaidut of Flame stabilization
on Gas Dynamic Scroons, by V., A, Kusteriu,,
A, Ya. Khismatullin. 14 pp.
RIZIHAN',, perm, IVUZ Aviatsionnaya Tekh, :4o 400
1%70 pp l14-17f.
AIIVI-"nj/1.,,r-24-428-60"
Sci/Prop F, Fuel
Nov 69 59S#958

I.kilactim ot tie 44iial NO: ad) iotio in We
WAOU :i),tilops 0l., lLiL.ol 'Aalpanktum. GEM 'AubbWas"
Lry V. 1. Ukall. 17 L,)p.
deri, IzW-,,-tiya VyssUkh UdK-I)nyldi
&xiwnix- ~Viataicmqyzl 'A4j*,alXa,, Jo 40,,
i967j, ,,) 123-133.
j'djVl"kl)/X16-23-1055-68
-3ci/4q.~Usiui aid fup-lo
juic 69 382j,970

Calculation of Rudders with Fillers, by
V. V, Yershov.
RUSSIAN, per, Izvestiya VUZ Aviats Tekh,
No 1, 1968, pp--M-43.
PTD- S - Oft ~ S'*? - (-- ~
Apr 69 380,281

Instability of the Zone of Turbulent Burn-
ing in a Rocket Engine Relative to a Change
in Us Its Lengths by S. K. Aslanov.
RUSSIAN, per, Izvestiya V1JZ Aviatsionnaya
Teklmika , No f, 1 68, pp 51-55.
PTD-S-2ft 6~
Jan 69 374,185

Cmipnpison of Single-Stag
.,a and rIVo-
3ti4;o Axial Air Mloroft'rblno Perfomence,
by -A4, S., Mstnlevloh, 10 pp,
RUSSIAN,, per, Isvestiva
i vysshikh
uchobom zavwToqz,, Serile Avintsionns;Za
TeIdmIR&o._Knzan', No 1. 1960v pp 97-104.
301P 01.0 369t240
Nov 68

Some Features of the Separation Process in
a Multistase Axial Compoessor, by
N. 1. Saposhnikov.
RUSSIAN, per, IZV VUZ Aviats Tekh, No 1,
1968, pp 105-1117-
FTD-S--Ir&-2- ,- c,
(L. /
Mar 69 376,164

optimum Expansion in a Jet:
Ye. D. Stenkin.
RUSSIAN, per, Izvestlya V1)Z
No 1, 1968, pp
PTD-S-4" 1,s-),
Mar 69
Nozzle, by
Avlats Tekh,
--
37811662

Investigation of the Ejecting Action of a
Turbdlent Jet by the Electrodynamic S~mu-
lation Method, by G. T. Aldoshiv,
G. V. Gindin.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 1,,
1968, PP 141.-lT!T.-
NASA TT F-12,136
Sci-Prop & Puels
June 69 383t228

Criterion
by V. P.
RUSSIAN,
1968, pp
FTU-S-5"
of Passenger
Koshkin.
per, Izv VUZ
28-32.
t,,1
Aircraft Efficiency,
Aviats Tekh, No 2,
May 69 382,366

lAminar Pawl Flutter ins Supersonic Flow. by
A, 1, Sadroov.
RUSSIAN, per, Izv VUZ Aviats Tek No 21, -,689,
L-11-0
pp 33-38.
CIA X-6804
Nov 68 3540073

Effect of Backlash and Friction on Self-Sustained
Vibrations of a Wing and Ailerm in Fli&OAq
by So 11. Struk1kovj A. 4, Kharlmov, and b,.,. b.
Novikova.
RUSSIM, per, Izvesti a Usshikh Uchobnykil
Zavedeni,X. Avd-~a Tekhnika No 2t 19680
;"p U-48.
ITD-S-30 /'- 6, 1~
Jan 69 3740343

The Instability Mechanismi of the Success-
ive Spontaneous Combustion of Fuel in a
Rocket )?.ngine Chamber, by S. K. Aslanov.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 2,
1968, pp 49-52 0
FTD-S-"+ ('~(' (
Mar 69 376,310

fixperimental Detormination of the Mean
Heat Transfer Coefficient. in Impluse
Blades in a Supersonic Ga.s Flow, by
A. F. Shtyrlin.
RUSSIAN, per, It VUZ AvivAs
1968, pp 78-84.
. k.
May 69
Tekh, No 2,
380,895

Analysis of Solid-Puel Rocket Engine
Efficiany by Test Results, by
2. P. Belking.
RUSSIANO per, Izv VUZ Aviat Tekh, No 2,
1968, PP 100-IU7-.
PT D - S -.3," -/(' - 6- ~
~'~ I . "', "17 - - 7,~'
z e~ 11 /L~ ( () "
r
Fab 69 375t400

Fb-d- Grid Within a Nonmifom %locity Field Flow
by B. G. Khudanko.
RU;SIM,, per,, Izv. VEZ. Aviatsiamaya Takhaika,
No 2, 1968p pp=6-J-32.
M-MI-Special 296-70
oct 70

(;f Aircraft aw
for i
ZLM,vl by i, v.
j.er.. Izv. %U/,. A%ii-ts. 'iWdin. Vol Ili,
"03,1 19
.6 8 16-22.
.W~~A Til !A-12,71)
sci/aarulautia;
z~)r 71) 404r494

Determining Aircraft and Engine Parameters,
Assuring Maximim Theroeticol Range at
Given Cruising Flight Velocity, by
1. F. Florov, 0. K. Yugov.
RUSSIAN, per, Izv VUZ Avi.2t3 Tekh, No 3,
1969, pp 50-53.
FTD-9-&%
~ I ') (" y
May 69 390,971

Gawralizatim of E)q3erivental Data cn Heat
Transfer, by V. I. IdW.
RMIMI, par,, Izvest&A VEX AviataiamayA Takhnika,
No 3, 19690 pp 67-78.
M HT Special 557-69
dec 69 398j,557

REQUE$T TR OHECK 21 -11 -11-jrY F3T69-1-2154T
Drag estimation in laval nozzles
B.S. Vinogradav, M.N. Makautoya
RUSS PER: IVVZ. Aviatsionnaya Tekhnika.. no 3.. 1968$
134-137

Experimental Investigatioa of Flame
Stablliz4tion in a Iligh-Temperature
Air Streato ot Reduced Pressure, by
Ye. L. Solokhin.
RUSSIAN, per, Izv VUZ Avists Tekh, No 3,
1969, pp 138-140.
FTD-S-3" (,,,/
Feb 69 375,403

I-bglish title unknown, by Yu. 11. Yakovlev.
[x!r, Iz. VUZ. Aviatsicnnaya lbklinika,
No 3t 1968, R) 137-149.
ITD Ill'Special 55&-69
Oct 69 395p3O5

Eng1ish Title Uiknown, by V. :1. Vormin, et al.
RUSSIM # per, Izvestiya VUZ. jWiatsicnnaya
'fekhnika, No 4, 1968P PP 59-69.
ETD irr Special 492-69
oct 69
393tO8O

Oscillations of Gases in Afterburners,
by R.G. Yakupov.
RUSSIAN, por, IVUZ Aviatsionnaya Tekhnika, No 4,
1968, pp 103-10.
FTD-HT Special 71-24

On Ono Method of Determining I'atiguo Lifo of Air-
craft Stnictures., by S. G. Muganlinskiy,
N. F. Chekhonin.
FdJSSIAN, per, IVUZ. Aviatsionriya tekhnika, No 4,
1968, pp 145-148.
FTD-HT Special 369-70
jan 71

Nonlinear Axisymnetric Vibrations of
Cylindrical Sholls Wound from Ilautic
Filazients, by A.M. Elpat'evskif & A.A.
Dudchenko.
RUSSIAN,per, IzV. VUZ Aviats, Tekhn.,
No. 1, 1969" I)P,, 14-:20.
CIA X-7097
Sept 69 391,378

on the Influence of Boundary Conditions on
tho Stability of a Cylindrical siiell
Loaded by External PreBoure and Axial
Tenaile Forces, By S.N. Han & V.L.
Ingulltsov.
RUSSIM,per, Izv. VUZ Aviate. Teklm.,
No. 1, 1969, pp. 17-31".
CIA X-7096
Sept 69 3910377

On the Problem of Experimental Determ]-nation of
Unit Conlitimpblot) Jiablo~ by .1 . A. D()hod(~Ych' :111d
N. B. llutovskiy.
RUSSIAN, per, Ivuz. Aviatsionnaya Tekhnika No 11
1969~ pp 56-62.
FTD HT Spod-A 71-63
mar 71

Q~aa mewhad for owtexmbkLoo the Opus"
Toubl" Paransiom adth L4nr Vblume Flow by
oq ff.~ Yomin. 12
No is 19"s pp 70-76"
MAU TT P%01209"
tow 70

Conjugate Problem of ueat wchangc, with
Radiant Ifeat lUchange Near Plate Surface by
Le I* Kudryashev. 13 pp.
MiSIMp parp Jay, Vvsahik)k Uchehn, zavedenii.
AvJ&As, MlWM,v 'No 19 1969g pp 77-84.
NASA TT F-12,981
T C'.
Usa
sci-Viex
nov 70

REQ TH CHEM 19-03-73 T373
INFLUENOE OF COOLING ON THE WORKING FLUID
PA4METERS IN AN AIR-COO.'.rED TURBINE STAGE
MAY, V I;KUMIROV, B A
UR:~ IZVESTIYA VYSSHIKH I]CHEBNYKH ZAVEDENIYD
AVIATSIONNAYA TEKHNIKA3, 1969, VOL 120 NO
1t PP. 5-92
FA

IWKcoct Vatbod of AT TIM
Womb lastdo CINAMA o4 abs la"Tatwe
to ftmt of Dodd* Plow Turbim by
No V, porwyehin, 9 pp.
RUSSIMp PQ3rV 7AMMMAL~4
AAOU- Ida-'s me It too I pp 93-M.
MM TT Pftl2p9B2
voo
"im"ro
ow 70

Gowzalimstion of Gradient Method of Heat
Tlr*mfor Investigatimse for Ww case of Arbi-
%way of the Tboxml Conductivity
CoeffWant of the ftll an ToWerature by
V. K. shawd 9 pp.
b! h I n haft haft
MIMI per$ F&AMO~-- snob
hdaum Id1hup 10 19691 pp 105-109.
NASA TT P-12V983
PY1" III', I "', ~ ,,~ -,T,
usa
sci-ther
nay 70

rietmilwUm of TodnUnt, Plow on PUt Pexpon-
diculax ObOx"Caft by
L A, BUIAWW* 4 pp.
amuse Pazt AWA.
ASIAMUM pp
MW TT r-120"4
now 70

Theoretical Determination Of the Discharge Go-
Offi-ci-al't (if Conv(~rsjetil. Cimir.,il Noz/,h-:;, by
B. M. Arontiv, Yii. I . T.-jybLzov.
RUSSI.IVN, per, Izvestiya VUZ AvLitsLontiaya Teklinika)
Vol 12, No 2, 1969, pp 41-48.
*PTI) 11T Spoci-.fl 136-70
May 70

On Calculation of Wave Proces.ses in Pipes when
Mling Them with Liquids, by V. 1. Yasin and
V. A. Yorudlin.
MISSIAN, per, Izvestiya Ylsshikh Uchebnykl~ Zaved-
eniy. Aviatsionna-ya Tekhnika, No 2, 19% PP 49-
55.
F'TD IIT Sj)()-cid 71--b'2
mar 71

Ttirbulant Boundary Layer in th(.,. Initial Part. of
the lli.pe During Hit- Blowing of Vari.ous Gask~ts,
by A. V, FaftirLnt J. D. Krechel;nikov.
RUSSIAN9 perk Izv VUZ Aviatsionnaya Takh, No 2,
1969, pp 79-88.
FTD IIT Special 150-70
Sci-Phys
June 70

) j j
aal.ciiIatiai (A ~mt ':),dw3non In Piiablor,kil
%Atli a Y3-cirejp by
yu, ll~ ~i*alovjev.
lzvr-.,Itiyzi VIZ, Aviattsininaya
'11--k?nLkap Alc) 2p 1-969, Ivp tY)-913.
TOI.`~A TP 1:' 122,974
.4 ly:Ac.-,

70-13585-IOK
Aryshenrik.'l. Vu. M. Kaltahskil. 1. L: Llv:irov. V. V.
CERTAIN PRODUNIS CONCERNING IME MkSTICITY
OF ORTHOTROPIC MEDLA. lzvestiya Vysshikh. Ucht-bnvkh
Zovedenfl. Avl4tolonnava Tekhnika, *e. 12, n. 2. p. 115-
Order trom NTCos 70-IJS8S-20K: HC $ 6.10. Mj-' $ 5.90.

Chiculati.on of: 11;mvieters when Real Gis Ls FlowLng,
by N. S. Yersh(m , V. S. St!litonov.
RUSSIAN, per, Izv VUZ Aviats T,aRhj No 2, 1969,
1.43-1,48.
pp
Li'rD 11T SpocLal 15t-70
se i.-Pllys
June 70

Modelling of Two-I)Lmensional Probl.ems of Flowing
wi.1.1i ';t.,i 1 1 hip. , by A. 1'. i'mitwti-vov.
RUSSIAN, pea-I Izv VUZ AvLats Tctkh, Nu 2, 19693
pp 149-153.
FTD HT Special 152-70
Sci-Phys
June 70

lx~ h!rm i.11.,It i.1)1-1 (If t III! ~1;,X j.j,.ljlljj I'(-j 1- 11 i q.,j j 1) 1 (1 WC, ' pJ1 I
1 1
I IC h'.11 i.gll Ou 1. 111 Y!1 1'() r . I V.~l I- i il 1) 1 1.! GI. (mw L ry 141 lip. ,
by V. 11. Gogti.n.
RUSSIAN, per, Izvestiya V1JZ AvL'atsiotiriaya Teklini-ka,
Vol 12, No 2, 1969, pp 169-171.
*P'11) 111' Spiwl.al 133-70
May 70

Optimum Control of Boundary Layer, by 0. G. Divakov,
T. K.
MISS I AN , pe r, 1, .-.vc--i ( i y~i V11,'. Av i.ii I :j i min.1y., TOkillk L1%;j p
No 3, 1461), pp 5-13.
*FTD HT Special 135-70
May 70

To Ow Probluit, 1,1' Laiiihiar Boundary Liiy(tr Steadi.-
noas t)E Noncomprcmji.bl(i Fluid in A(.-(,()mi1 ()[
Trawliverav Spou-d) by :.I. V. Tzvo.Lkov~i.
RUSSIAN, per, 1zv VUZ AvLILS rekh, No 3, 1.961),
pp 33-40.
M,'D HT Special 153-70
sci-Phys
June 70

Karasev, ON.
Determining the Angle of Downstream
Flow from a Two-Dimensional Irbine Blade
Row.
IZVESTIYA VYSSIKH UCIfEBNYKH ZAVEDENII,
AVIATSIONNAYA .TEKHNIIIA, N. 21 19681
P. 66-71
NTC- 72-14627- 20D
Feb 73

REQ 11,11 C1,11ECK 20-03--73 T375
CALQVLATION OF THE TEMPERATURE FIELD OF
C00L9D TORBINE BLADES FOR VARIABLE BOUNDARY
COND~TIONS AS A FUNCTION OF THE THERMOPHYSIC
PAOPtRTl#S OF THE 14ATERIAL AND THE
TEMOERATURE
LOKAks V:ol
UR; IZVESTIYA VYSSHIKH UCHEBNY KH 'IAVE*NIY,
AVlATSIO*AYA TEKHNIKA, i969, VOL 12, NO 3a
pp. 80-19p

i4s V -
i
1
G
1

Study oE a Diathermic
";(. III lilv, IA: I l,.,!1 I, T I % I I I: I I 4~v wi th :-'-u p., rrri I ic~i I Rt~vjmo
of Boil.Ltig,I by Yu. 1'. yjjk(.)vlttv~ V. N. Drulin.
RUSSIAN, per., Izvestiya VUZ AvLatsLoiiiiayajckliti~ka)
No 3, 1.069, pp 91-96.
*l"'I'D Ill' SI)O.Ci..'ll 13~1-70
May 70

Influolluo of W14) Oyatum (1.11"Onalon"I ()f* 1J1o
characteristics of the burning process, by
V. M. Yankovskiy, A. V. Talantov.
RUSSIAN, per, IVUZ,- Aviatsionnaya Tekhnika, No 3,
1969) PP 97-107
WD-HT Special 371-70
sca.
jan 71

The Influeme of Transverse Pressure Gradi.ent on
Till'billwil llollllll~iry I.nyor 1).N
G. V. V1.1i.ppov, V. C. ~Awikhijv.
RUSSIAN, per, Lzvestiya VUZ AviatsiomiayLi I'Ahilika,
No 3, 1969, pp 145-149.
*i.rri) in 134-70
May 70

Lxperimental Investigation of Toroidal
Shell Stability, by Yu. A, Fedosov.
RUSSIAN, per, Izvestiya Vysshikh Uchebnykh
Zavedenii. Aviatsiopa P
..ja _Tekhnika No 3.,
1969v pp 154-157,
NTC-70-13156-20K
60 Ze~' .-7 3 k
Feb 72

DetezwInation of Stress and Strain Components in the
Mwtio Complex Stressed State, by Lyeov H. 1.
OMAN., per.. Ivuz. AviatsionnaUa Tekhnikq,
1969,g No 4,, Vol 12, pp 43-50.
FTD-UT-Special 71-70

Theoretical Perfoxinance of a Turbojet Engine Nozzle
which has a Center Body with the Presence of Blowing,
by Z.G. Shaykhutdinov.
RUSSIAN. per., Izvestiya Vysshikh UchebnXkh -Zoavedcniv),
Seriya "Aviatsionnaya 'rekhnika", No 4, 1969, I)p 91-97
FTD-1-11' Special 71-31

Calci~Lation of a fuo-1 dr nozzda,by,
1. N, Dyatlov.
RUSSIAN, per, IVUZ. Aviatsiomaia Tekhrdka, Vol 12,
No 4, 1969, pp 153-137.
FTD-11T Speci,,a 3597-70
jan 71

Calculation of the adhesive bond of an air-
craft structural joint, by N. Kh. Gizatulin
and So So Krestovskiy.
RUSSIAN, per, JV1JZ4 Aviatsionnava Tekhnikaj,
Vol 12, No 4. 1969, pp 158-161
FTD I-IT Special 327-70
sci
nov 70

Tr ff'T77
Fill
TV"
45
sTi
AIVY"& FIAM STABILIZER5
St4WAY-i'llitill in., 1969.,
--Ott
it m
o,

Prospects for Cooling with Diathermic float
Exchange Systemsv by Yu, P. Yakovleve
RUSSIAN.. per.9 JVUZ, AyiatsLonnav& TW=ikal
No 19 19702 pp 28-42
FM I-IT Special 321-70
nov 70

J.97-0p
t;~:, j,~ t;,
e, 4
aj
. . . ......

14ame Propagatic.)n Velocity in Turbulent Plow
Under Two-Stage Combustion, by V. A. Shchukin,
A, V, Mosin,
RUSSIANp per, Izvestiva Vysshikh UchebnvjQ
Zaygdelliv, Aviatsionnava lekhnika, Issue 1,
1970, pp 138-146,
FTD HT Special 304-70
nov 70

rl" ,
TT35
ON OF STba w6v nocressss
T X
TSIOMMIA, TXXW~ M-, 1970., vol 13,
1-19
4;:,
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OJI Cylindrical Prof iles of a Centripet.-al
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NASA-T-F-F-14060
Nov 1