RUSSIA AND UP FR: IZVESTIYA VUZ AVIATSIONNAYA TO: IZVEST VUZ, AVIATS TEKH

• Document Type: CREST
• Collection: Consolidated Translations
• Document Number (FOIA) /ESDN (CREST): CIA-RDP84-00581R000300950022-7
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 84
• Document Creation Date: December 29, 2016
• Sequence Number: 22
• Publication Date: December 31, 1972
• Content Type: ABSTRACTS

Determining the Basic Parameters of an Air-
craft Whoun Flight Path Incluclas it Low-
Altitude Flight Phase, by S. Yu. Skripnicli-
anko.
RUSSIAN, per, izvestiya VUZ Aviatsionnaya
Tekhnika, No 3, 1967, pp 110-116.
MD-S- .
Jan 69 374,183

Rulation lietween liciht I'lesistwice and cost
lor v Wo-Stage Nairocavorable Space Rocket,
by A. A, Kuznatsov,, 10 pp.
PUSSIAN, per, IVUZ, Ser Aviat Tekh Vol 10,
No 4, 1967, pp 9-1S.
AR~J/RSIC/Tr-888-69
Sci/Space
Apr 69 377,419

~;I;ribillty of' 'Iwo-DIvionnional 1~'oundax-y-
Layer Plost of an Incompressible Pluid
in the Caso of Small Accolorations,
by III. N'. Ilikitinp 13 pp.
~)Gr VU7 Avints. Tekh.,
1 2 -9 Izv.
Vol 10, 11o 11, -1967; n-p 16-23-
Dept of lfavy APT,/JIITJ T-2154
sci/P~qs 368,935
Oct 613

Effect of Flow Boundaries on the herodynamic
Characteristics of a Mmg at a Nanstationary
Movemint, by Z. Kh. Nugmmcyv, 5 pp.
PUSSIAN, per, Izvestiva VUZ. Avlatsiannaya.
Takhmika, No 4-,-D'O, pp 24-N.-
pm-,g:-,Vs y ("Y - (' C'
469-69
aug 69 388,565

On the Problem of the Synthesis of Optimal
Control of Elastic Flying Devices, by
T. K. Sirazotdinov.
RUSSINA, per, Izvestiya VUZ Aviatsionnaya
Talhnika, No 4, 1967, pp 50-40.
FTD-S-3" 6/- -, ~
Feb 69 375,398

InvestLyaum of tile Effl~ct c7f ijisd-lart
-p-
Cx)oliii,.j iAr Illacb.,; into t-l-K,! ;?a(Ual
Clei~waiau-s (x*t tlia U~ lkabirw LUvju (jx3raLLai,
b1? YC. N. IXKJCVCaDV. 3-5 1)1-).
im'sim, r, Izvesti-Ya -kN-,,-,Iiikh LTd-k--vnyMi
Z avwe . 0 Aviatsicnnaya '.Ltkliriika I'lo 4, 1967,
vp 69-78.
7a IVETA)II. Z1-2 4-2 4 8-6 8
sci/pqysicn
apr 69 177 -n1 -1

'Zic ;-,cosibiliLy of Auulating CaNdtatim
ill"- iu u4 ia in 'Ib-Aintj U--aiLiii:,.xkjU Pui;p-, on Gmas,
jjy .1j. ~'. Ykjr.,~ajlLw. 13 pl).
ldl;SIRA, per, Izvestiya Wsdlwl ud-telvl ;j1
zavea.u * . lv=tsictuiaya lidduilka, 10 1967
pp 79-87.
.t U lVVII011 rX6-23-1093-68
sci/lIedim eaijr
junu 69 382,985

l2w ~-xmsticn of lzq3erivental inw-stigaticn of
Sqjrumcnic 'Itubine Cascadas, by
V- 13- Pallf:ilOViCil- 8 LJP-
141-kilhl, per, Izvestiya Vyssld.U"i Ucbevnvkh
zavedeniy. jA~j=tsiMnaya_ME4duAka, No 4, 1967,
pp 102-107.
Al PATIDIV 116-2 4-2 4 0-6 6
sci/propulsim and fuals
apr 69 377,918

'.' -uu-lix!iiu2 of Ermrm; in 1:1ai
i~actLUO Ql ble Lavor, -IkNlo~ of ..,I"tocl (lizinicte-l-
j.!;tia; oc 'WLix)jet i~vjxxn (TA)) , by
lzvu~,,*tiva NAZ. A~.jtcdonnqya
rAkluiika Ao 4, 1967, pp 124-129'.
Scd./ pl-IoPulsicn mci fuals
act 69 395,323

Constructing the Supersonic Part of a
Nozzle by Given Velocity Distribution,
by V. M. Fomin.
RUSSIAN, per, Izvestiza VUZ Aviats Tekh,
No 4, 1967, pp 130-136.
FTD-S-4,13q,1se 6!C1,
Mar 69 378,616

Dotollidliation of UIC
]?%-oqu,oncios of f1hells Of COMI~ACCC SII,-IP0
'.-litli 1'ree Edges, by G. 1-1. Saulnikov,
A. G. 'Z'emikov.
RUSSIAN, per, -Izvost ya VYSSI-aldi
Uchabnykh Znvodal Aviatsiolmv.-a
It
Vol 10, 110 4, 1967, 'rip 143-348.
I-TA SA -11,719
Sci/Aaro .369,121
oat 63

On the Equation of Relative Weights of an
Aircraft, by N. A. Fomin.
RUSSIAN, per, Izv stya VUZ Aviatsionnaya
i"ne
Tekhnika, No 4, 67, pp 149-154.
AIR7FT-D7MT-24-348-68
Sic-AeTo
Apr 69 380,33S

Weightlesanew and ArtiXicial Gravitation,,
by T&I lit, Shapiro*
RUSSIATI,p perj, IEMaW bM&Zb UcbebMa
M&A4 WA
Vol JLOs :110 4s 39b7s ]PP J55-aWl
M%8A TT INAX7
SOL
Doe 68 371o244

ui Ux-6usLion in kIct-T, 1 P_V. 'ralmtxw.
-)or IZVOS. ya WSW)ikh UdiclAl kh
L 0
zaved U., Avjat:.qicnn~ya 'AAduLika, Jo 1967,
;pp 5
ATIVVIDA, 511-24-209-68
,Aj 41 ( _~-se, 19 ~
Ll/
sci/px)pulstion and Elm-Is
~;qy 69 381,121

Inw-stigaticn of Flcx.; Interactiai During the
Injacbbn of a Gew into the Suparscnic Socticn,
by 13. S. Vinogradav.
RUSSIAN, per, Izv. VEJZ. Aviatsionnaya Tekhnika,
1:9F.-
No 40, 1967, pp 9
ETD-IM-Special 297-70
oct 70

i1, I-':)'tIIdy of tile Nuchal'islu Of 11~Lae 'Aabilizatioll
on Gas J)ynamic Screens, by V. A. Kosterin,
A. Ya. Kbismatullin, 14 pp.
RIA'361AN, per, IVUZ Aviatsionn.aya Tekh, No 40,
1967. pp 114-172-.-
Al R/j-m)/,.-,r-24-42 8-68
Sci/Prop & Fuel
Nov 69 395,958

-~.Jljactiul ot tv.- q7itil'al (U/C- ,d) 41~atio in tiu
W)Liti Sta4:is oj: iii,)i '!bq)orzituxr-- GEL, ixubhioo,
by V. .1. Lckay. 17 pij.
lUklUil, per, Iz%es ya !~Z~Iikh Udiebnykh
Zzxku", y._ , ANviatsicnnayi 'ibldrakaL.Jo 40, '
.WU7, ip 123-1~U.
sci/j>mpulsicti anci finis
juw 69 382,r970

Calculation of Rudders with Fillers, by
V- V. Yershov.
RUSSIAN, per, Izvestiya VLIZ Aviats Tekh,
No 1, 1968, pp 35-43.
FTD-S-94* / g'-3 - (--~
Apr 69 380,281

Instability of the Zone of' Turbulent Burn-
ing in a Rocket Engine liclative to a Change
in 23kx Its Length, by S. K. Aslanov.
RUSSIAN, per, Izvestiya VVIZ Aviatsionnaya
Teklinika , No 1, 1968, pp 51-55.
ETD-S-2xc 23Q-Le
Jan 69 374r185

Cork),irinon of Singlo-stago and Two-
Stago Axial Air Mioroturbino Parforranneo,
by A# S, Hatolevich, 10 ppt
RUSSIATT, per, Izvestiva v-vsshikh
uchebralch zave UMFIY. SW~ Aviatsionnaya
Tekhnika, Kazan', No 1, 1966, pp 97-104.
JPUS WO
Sai/Aoro 369,240
Nov 68

Some Features of the Sepayation Process in
a Multistage Axial Compwossor, by
N. I. Sapozhnikov.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 1,
1968, pp 105-11-1.
FTD-S 3,82
Mar 69 376,164

Optimum Expansion in a Jet Nozzle, by
Ye. D. Stenkin.
RUSSIAN, per Izvestlya VUZ Avlats Tokh,
No 1, 1968, ~p 112-119.
FTD-S-+" 6c1
Mar 69 378,662

Investigation of the
Turbulent Jet by the
lation Method, by G.
G. V. Gindin.
RUSSIAN, per, Izv VU3
1968, pp 141-14-5.
NASA T97 r-12,136
L'jeciling riction of a
Llactrodynamic Simu-
T. Aldoshiv,
"iats Tekh, No 1,
Sci-Prop & Fuels
June 69 383,228

Criterion of Passenger
by V. P. Koslikin.
RUSSIAN, per, Izv VUZ
1968, pp 28-32.
FTD-S-544 (.7'-/
Aircraft i-ifficiency.
Aviaits Tekh, No 2,
May 69 382,366

Lwninar hanal Flutter ina Supersonic Flow, by
A. 1. Smirnov.
RUSSIAN, 1-.)er, Izv VUZ Aviats Tekh, No 2, 1968,
pp 33-38.
CIA X-6804
Nov 68 354,073

Effect of Baclclasit and Frictim on Self-Suitained
Vibr;xti(xl.,. of a wlinv mid Ailorm in I'liclit,
by S. 11. I;trcklkov. A. A. Kharlsimov, and M. B.
Novikova.
PAJSSIAN, per, Izvestiya Vyssh kil-Uchobityk-li
Zavedeniy. Aviatsiannnya Teklinikat No 2, 1963,
7p 39-48.
FTD-S- SM / - & 5
Jan 69 374,343

The Instability Mechanism of
ive Spontaneous Combustion of
Rocket Ungine Chamber, by S.
RUSSIANS per, Izv VUZ Avis-ts-Tekh,
1968, pp 49-52.
FTD-S-3:V+ (,7(;, 6~
the Success-
Fuel in a
K. Aslanov.
No 2,
Mar 69 376,310

Experii-nental Detormination of tile Hean
Iloat Transfer Coefficielit in Impluse
Blades in a Supersonic Gas, Flow, by
A. F. Shtyrlin.
RUSSIAN, per, Iz VUZ Aviats Tekh, No 2,
1968, pp 78-84.
FTV-S-54e&,c~ - ~-q
May 69 380,895

Analysis of Solid-Fuel Rockot Engine
Efficiany by Test Results, by
Z. P. Belking.
RUSSIAN, per, Izv VUZ Aviat Tekh, No 2,
1968. pp 100-107-.
FTD-S-.-,"
70
Fab 69 37S,400

Ibd Grid Within a Nonuniform 'Vblor-ity riold rlcw
bY B. G. 1(hudenko.
RLSSIAN, per, Izv. VLIZ. Aviatsicnnaya Tekhnika,
No 2, 1-968, W-M--132.
FTD-Hr-S-Imaial 296-70
oat 70

i I "'i
Illaticik of rcral't 'Aillu ih''J-no
.1 . *.-W.:-ILL,~ 5ik-.orkttic~ll j-(-)r -I
i;im;-ii cruisblj by 1. P. Plorov,
OJ. K. LuLjov. li*pp.
RWISIX-4, per, Izv. MB. Avi,7d-s. 'Ibldin. Vol 11,
No3, 1968, pp 16-22.
'Jiv.;A Tv 1-12,732
scm/aermautia3
70 404,494

Determining Aircraft and Ei,-tgine Parameters,
Assuring Maximim Thorootical Range at
Given Crui3ing Flight Velocity, by
1. F. Florov, 0. K. Yugov.
RUSSIAN, per, Izy VUZ Aviats Tekh, No 3,
1968, pp SO-53.
FTD-S - S-54 :~) -:2 3 - 6 9
May 69 380.971

Guseralizatiai of Experinmtal Data cn Heat
Trawbur, by V. I. Ickay.
IW),SLVI, per, Izvastiya VLIZ A,,datsicnnaya Takhaik :EL
No 3, 1968, PO ry-7c-
ETD HT Special 557-69
dec 69 398,557

REQMST TR 011ECK
21-11-M&Y RT61/1-.1-23-54T
Drag eatimtion in laval nozzles
B.S. Vinogradov, M.K. Makautova
RUSS PER: IVUZ. Aviatsionnaya Tek~mika, no 3, 1968,
134-137
/9

Experimental Investigation of Flame
Stabilization in a Iligh-Temperature
Air Stroam at Reducad Pressure, by
Ye. L. Solokitin.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 3,
1968, pp 138-140.
FTD-S-3S* 0- G9
Feb 69 375,403

Fliglish Litle unknown, by Yu. 1". Yakovlcv.
RUSSIAN, per, Iz. VUZ. Aviatsicnnaya 'IbMinika,
No 3, 1968, pp-MMT.-
IFTD IIISpecial 558-69
oct 69 395,305

English Title Us-known, by V. I. Voranin, et al.
RUSSIAN, per, Izvestiya VUZ. Aviatsicnnaya
Tekhniki, No 4, 1968, pp 59-69.
ETD 11T Special 492-69
oct 69 393,080

Oscillations of Gases in Afterburners,
by R.G. Yakupov.
RUSSIAN, per, IVUZ Aviatsionnaya Tokhnika, No 4,
1968, pp 103-107.
FTD-FIT Special 71-24

On Ono Mothod of Determining F-i-Liguo Lifo of A:Lr-
craft Sixuctures, by S. G. Mug,~uainskiy,
N. F. (2iekhonin.
FUSSIAN, per, IVUZ. Av�atsioni3,)2 tekhnika, No 4,
1968., pp 145-lIT8-.
FTD-HT Special 369-70
j an 71

onlinc-ar Axisymnetric Vibrations of
Cylindrical Shc113 lolound from 1-:lastic
Filaments, by A.N. Upatlevskif & A.A.
Dudchenko.
RUSSIM,per, lzv. VUZ Aviats. Tekhn.,
No. 1, 1969, pp, 14- 0.
CJLA X-7097
Sept 69 391,378

On the Influence of Boundary Conditions on
tj)a StabiliLy of a Cylindrical Shell
Loaded by External Pressure and Axial
Tensile Forces, By S.N. Kan & V.L.
Ingulltsov.
RUSSIAZI,per, Izv. VUZ
No. 1, 1969, pp. 27-33.
CIA X-7096
Aviate. Teklin.,
Sept 69 391,377

On the Problem of Ikporimental Determination of
UnIL ConowiijAdon Ratio, by 1. A. Doboduyuh-, wid
N. B. Rutovskiy.
RUSSIAII, per, Ivuz. Aviatsionna.Va Teldmika., No 1,
1969, pp 56-62.
FTD IIT Special 71-63
mar 71

General Method for DetemIning the Optimal
Turbinia Parameters with Low VaImme Plow by
00. No ye"n* 12 PPOL
RUSSIAN& perg Imr, wash. Duak, zaudsm.
,p 70-76.
Aj&L",_j~kLug No ls 1969, 12
NASA TT P-129900
mi-C, 7 a - I I
uSI&
*eA-aex,o
nov 70

Conjugate Problem of lieat Exchange with
Radiant Heat RKclianga Near Plate Surface by
L. 1. IUdryashev. 13 pp.
IZLISSLVq,, per, Izv. Mysshilch yr
,_Iiebn. ?,avedgaii,.
&IatM.--MW"m 0, No 1, 1969,9 pp 77-84.
F-12,981
us&
sci-their
ncrv 70

w
dd
On 'ZT 'IOA '6961 'VMINHMSI UVNNOI9lVIAV
7,INHCI:-IAVZ HMTN92H0n HMI14SSXA VXIISSAZI : W1
v 9 cAOUIlTnM!I A 9A VM ON
I-ovis sNiaiini CIT1000-ITIV NV NI Sll5l&!IHV3Vd
aIn7A ONIMMOM HH'5 NO DMIqOO3 90 90N:ilflrJ.!TNl
ELFS, ILT. ~IFlll

lndir*tot blethod of Determining Air Flow
Through Inside Channel and Gas Tewerature
In Mat of Double Flow Turbine by
N. V, Pervyshin. 9 pp.
RUSSIAN,, per, IN& Vvm~AW"1W&dM" 79KNO11211U46
AML&U--Tekhn,,j No 1v 19690 pp 93-98.
NASA TT F-12&982
us&
0"-&elro
nov 70

Generalization oZ Gradient Method of Fleat
Trans.fer Investigations for the Case of Axbi.-
trary Dependenco of the Tharmal Coiuk%ctivity
Coefficient of the wall ort Temperature by
Vo K* Shcukin. 9 pp,
RUSSIAN, per, Ism, )tZeshith jt2hebn- Zayedpaiji.&
63CIA go Xfta-, No -11, 1969, pp 105-109.
NASA TT F-120983
t"k-l-c' -1;j - / q 3 q'5' - R 0 M
usa
Oci-ther
nov 70

Distribution of TUdalent Flow an Flat Pezpen-
dL*ular Obstruction by
IL A. jualanev. a pp.
RUSSYMI per# in- 2ULWAM gods, lav2dwilu'..
AXWOM SAMOA., No lp 1969# pp iis-Ile.
RUA IT P-13,94
9'r Q. -;t oz,
IMS&
WA -aere,
Itkow 170

- ~7-
T*R,'(!HECK
(MS FLOWS HAVING A MOD4111TO1,11 PC).PE"FVJ'TAb
FABRIKANT N YA
U'R': PfUZ. AVIATSIONN-AYA TEIC-E\TIKA
2, pr,) 1.5-22

Theoretical Determination of tha Discharge Co-
oCCic.Lent. oC Convergwit; Conixal Nozzl.~!:;, by
11. M. AV011OV, Yt1. L. 'I'Sybi.ZOV.
RUSSIAN, per, Izvestiya VUZ Aviatsionnaya Tekhnika,
Vol 12, No 2, 1969, pp 41-48.
*FTD 11T Special 136-70
May 70

On Calci;LLation of Wave Processes in Pipes when
M41ing Them with Liquids, by 11. 1. Yesin and
V. A. Yermilin.
RUSSIAN, per, Izvesti:ya Vysshik-h UchebrXVkh Zaved-
eniv. iatsionnaya Tekhnika, No 2, 1969, PP 49-
55-
FTD HT Special 71-62
mar 71

Turbult"111: Boundary Layer Ln the Initial Part of
the PLpe During the Blowing of VarLous Gaskts,
by A. V. Vafurin, J. D. lkrachetnikov.
RUSSIAN, per, Izv VUZ Aviatsionnaya Tekh, No 2,
1969, pp 79-88.
FTD 11T Special 150-70
Sci-Phys
June 70

Yu. ll~ \fzuiovji--v.
RUiSIAA, Ix-or, Izvu--t-iya VLrZ, viatsictulaya
'kak!v,%!Rn, No 2, 1969, 1-yp 39-96.
P 12,974
sci/physics-
q3r 70

70-13585-20K
Aryshen-MI, Yu. M.; Kahaliskil. 1. 1.; Livarov, It. V.
CERTAIN P1103LEMS CONCERNING THE FLNNI-IC17Y
OF ORTHOTROPIC MEDIA. Izvestlya Vysshikh Uchebn%-kh
Zavedenil. Avlatsionnaya Tckhnika. v. 12, n. 22. p. 115-
Order from NTC as 70-13585-20K: HC s 6.70, NIF 1, 5, 80.

CLaculati-on oE flaramaturs when Real. Gas is Flowing,
by N. S. Yurshov , V. S. SeliEunov.
RUSSIAN, per, Izv VUZ Aviats Tekli, No 2, 1969,
pp 143-148.
VrD IIT Special 151-70
Sci-Phys
June 70

Modell Liig of Two-DLllensL.)na1 Problems of Flowing
wi. 1;h -;I ii I I imp., by A. 1'. I'll doviiyov.
RUSSIAN, par, Lzv VUZ Avi-ikLs Takh, No 2, 1969,
pp, 149-153.
FTD HT Special 152-70
Sci-Phys
June 70

OE 1:110- Maxi.1mim Permissibi(' wcij-jit
(If IMNLI!.11 0111.111y:i EOV .1 Vill'i.111)h, 14i'lig,
by V. P. Guglin.
RUSSIAN, per, Izvestiya VUZ Aviatsionnaya Tek-hnik-a,
Vol 12, No 2, 1969, pp 169-171.
*17'ri) Iff SpcciaL 133-70
blay 70

Optimum Control of Boundary LayE~r, by 0. G. Divakov,
T. K . syr-,Iso , (I i.il(.v .
RUSSLAN, por, L~wLi:Ai-pi Vtl/, AvLiLtii.ojinay~i TL!I,.hIILka,
No 3, 1969, pp 5-13.
*FTD IIT Special 135-70
May 70

To 1-1w Prob)u-m of Lami.nar Bound,'iry Layer Steadi-
nus.s ot NotwumprussLbtu Ftui.(] Ln AccounL of
Tvansvur.,je. Speed, by M. V. Tzvetkova.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 3, 1969,
pp 33-40.
F'fD IIT Special 153-70
Sci-Phys
June 70

Karascv, O.V.
Determining the Angle of Downstream
Flow from a Two-Dimensional Trbine Blade
Row.
IZVESTIYA VYSSIKH UCIIEBNYKH ZAVEDENII,
MFIATSIONNAYA TFKHRI]CA,, N. 2) 1968,
V-. 66-71
NTC- 72- 14627- 20D
Feb 73

HEQ TH CHECK 20-03-73 T375
CALCULATION OF THE TaIPERATURE FIELD OF
COOLED TURBINE BLADES FOR VARIABLE BOUNDARY
CONDITWONS AS A FUNCTION OF THE THERMOPHYSIC
PROPERTIES OF THE MATERIAL P34D THE
TEMPERATURE
LOKAY, V.T
UR: IZVESTIYA VYSSHIKH UCHEBNYKH 'ZAVEIVNIY.,
AVIATSIONNAYA TEKHNIKA, 1,969, VOL 12, NO 3,
pp. 80-90
-036(

Study of a Diathermic
schu-tilk" (if: lloill. TrilliffCct.- with Stili~!rcriAk:al ReVi.inct
of BoLling, by YLI. 1. Yttkuvtev, V, No Drulhq.
RUSSIAN, per, Izvestiya_VUZ Aviatsionnaya Tekhnika,
No 3, 1969, pp 91-96.
*VTD 11T Special 138-70
May 70

a .1. - i "'ll
jYj.rjjlWjl,tJ Of LII(J 0YOLCUll ()J' '110 PV"'(' -P
characteristics of the burning process3 by
V. M. Yankovskiy, A. V. Talantov.
RUSSIAN, per, IVUZ. Aviatsiormaya Tekhn:Lka, No 3,
1~69p P:p 97-107
FTD-HT Special 371-70
sci
jan 71

The Influence of Transverse Pressure Gradient on
I'LIT-JAIIA110 140111141"Iry 1"'Iyor Pa 11-Ors, by
G. V. Vitippov, V. (~. Slinklit)v.
RUSSIAN, per, Izvestiya VUZ Aviatsionnaya Tekhnika,
No 3, 1969, pp 145-149.
*FTD 11T Special 134-70
May 70

Experimental Inveatigation of Toroidal J-J,
Shell Stability, by Yu. A. Fedosov. 3 ,
f
RUSSIAN, per, Izvestiya Vysshikh Uchebnykh
Zavedenii. Aviatsionnaya Tekhnika No 3,
1969, pp 154-157.
NTC-70-13156-20K
(;Ij-q 7.Q-131S-Q,-;26K
Feb 72

Determincition of Stress and Stn2in Components in the
Plastic CompLex Stressed State, by Lysov Al. I.
RUSSIAN, per., Ivuz Aviatsionna-Ya Tekhnika,
1969, No 4, Vol 1211, 43-50.
FTD-HT-Special 71-70

Theoretical Performance of a Turbojet Fngino Nozzle
which has a Center Body with the Presence of Blowing,
by Z.G. Shaykhutdinov.
RUSSIAN, per, Izvestiya Vysshikh Uchebnykh Zavedeniy,
Seriya "Aviatsionnaya Tekhnika", No 4, 1969, pp 91-97
FTD-11T Special 71-31

Czalculation of a fuel -dr noz2ae,by,
1. N. Dyatlov.
RUSSIAN, per, IVUZ. Aviatsionnaia Tekhnika Vol 12,
No b, 1969, pp 153-157-
ETD-HT Special 397-70
jan 71

Calculation of the adhesive bond of an air-
craft structural joint, by N. Kh. Gizatulin
and S. S. Krestovskiy.
RUSSIAN, per# IVUZ. Aviats onnava Tekhnika,
Vol 129 No 4, 1969, pp 158-161
FTD HT Special 327-70
sci
nov 70

REQ T11 CHECK 3,-'Li-25 w84
INVESTIGATION OF COMBUSTION IN THE
AFTERBURNER ClWMER OF A TURBOPROP
ENGIM,i' WITH AIR FUEL FILAME STABILIZERS
BULAVICIN -A A
UR: rTUZ. AVIATSIONNAYA TEMNIKA, 1969,
rir'4, pp 59-67
71-

Prospects for Cooling with Diathermic float
Exchange Systems, by Yu. P. Yakovlev.
RUSSIAN, per, IVUZ. Aviat�ionnava Tekhn:Lka
No 1, 19702 pp 28-42
FTD HT Special 321-70
nov 70

All h=Wl*d* JbvtAaa vir X%ild Ailic.11-molio
Iry V. ii". X-mmall, v. 11.
. AM L
.K. A~D 11 ~1370
22 to: Titl2m.
MUR131MI r , I%p
lip
SWb 7D

Flame Propagation Velocity in Turbulent Flow
Under 'INvo-Stage Combustions by V. A. Shchukins
A. V. Mosin.
RUSSIAN, per, Izvestiva Vysshikh Ur-hebnvkh
Zavedeniv, Aviatsionnava Tgkhnika, Issue I,
1970s pp 138-146.
FTD HT Special 304-70
nov 70

REQ TR CHE6,'C
OT)TIMr,"ATION OF STOCHASTIC PROCESSES
SIRAZETDINOV T K
IVUZ. AVIATSIONNAYA TEKIRTIlCk, 19*-.-,,), vol
2.. pp li-19
71- 1;7

Unsteady Heat Conductivity of a CYlIndrical Wall for
A Vexiable Heat Transf ...... by yu. V. Vidin.
EMSIAN, per, Izvestiya.VUZ. AvintsionnWa Tekbn:Lka,
No 2~ 1970, --OP 52-57.
*FSTC-HT-'g!3-io47-72
Dec 71

The Nonstationax7 TemTembure Fields of the WKU of a
Pipe and the Heat Carrier cor Small Velues of the Bi
Criterions by B. M. Galltzeyskiy, G. A. Dreytser, 12 p-D.
RUSSIM, Pur, Izvestiya VUZ, Avia:bsionmM Tekhnika,
No 2j, 1970, pp 90-98.
AWqFSTC/Ur-23-15-72

Determination of the Aerodynanic Churactoristics
of an Faastlc Swept Wing in Stibsonic Flow, by
A, Kh. Karlmov. 15 PP.
RMSIAns, per, Izv, Vysshlkh Vchebn, Zavedenll,
Aviats. Tel0m,_ Vol J!r, I =o, PP 3-13.
4-71D q A - ~ 3 -- ee c. - '~/
VIC /Z.? 6,70- 0//)
-Oct 71

Avdeev, V. B,.
Experimental Study of the Enerfy Losses of
A Radial Flow in a Rotating Circular Cascade
of Cylindrical Profiles of a Centripetal
Turbine Rotor.
IZVESTIYA VYSSHIKH UCHEBNYFII ZAVEDENII.
AVTATSIOXNAYA TEKHNIKA, p.75-85
VTE-72-14628-20D
feb 73

RE'Q CHECK 20-03-73 T377
EXPER-, IvIENTAL INVESTIGATION OF TURBINE STAGE
14TTII AN EXHAUST OF COOLING AIR INTO THE
P LOW AREA
LOKAY, V I;KUMIROV, B A
UTZ: *EZVESTIYA VYSSHIKH lJCHEBNYKH ZAVEDENIY,
AVIATSIONNAYA TEKHNNKA, L970, VOL 1_6, 140 3,
Pi~- 93-100

---- TR : CIMCK----
.jtzQ
LOCLATI-0,N1 OF
A
FLA?
PATE Ka I T S
UR: IVUZ. AVIkTSIO!qD',AIZA
197CI, nr 4, I)P
=2A --5 -30
- - - -51
IFT filoli V),V VrNf; W*1"I'll A
Ij-
TE11URTIF-A
10-15

EEQ, TR CHECK C, -1 -26 TAEi
INFLUENCE OF SOME DESIGN PArtkMETERS OF GAS
TURMINE ENGINE COMBUSTION CHAMBER ON THE
CIRCUMFERENTIAL NONUNIFOMIITY Or, THE GAS
SPIRIDONOV YU A
UR: IVUZ. AVIATSIONNAYA TEKHNIKA, 1970,
nr 21, ,,pp 80-86
-Id
141 S
LIN

I ]'Pi I 1-1j"f . I [~.J' I" Il.". I, I 1,, -.1 I-P I I I - -1- 1" "
Expansicin of a Turbulenti-jet houndary Layer in a
slipst-rumil, by V. K. Temilov.
RUSSIAN, per, IVUZ Aviatsionnaya Tekhnika, Vol 13,
No 4, 1.170, pp 111-115.
NASA-17-F-14060
C)
Nov 71

f~f,f~, r-l~ cjlf"cl~
ITRICDIC FLUID FLOW THROUGH ORIFICES
SHORIN *V 11
UR: IVUZ. AVIATSIONNAYA TEKHHIKA
1970, vol 13, nr 4, pp l16-12i
p u

.... .......
Natural. Vibrutions of a Cylindrical Shell with
Elastic Core, by B. A. Korbut, 6 pp.
RUSSIMI, per, Izvest VUZ, Aviats Tekh, No 4, 1970,
pp 137-141.
X-7470
June 71.