RUSSIA AND UP FR: IZVEST. VSESOYUZ.NAUCH.-ISSLED TO: IZVESTIYA VYSSHIKH UCHEBNYKH

• Document Type: CREST
• Collection: Consolidated Translations
• Document Number (FOIA) /ESDN (CREST): CIA-RDP84-00581R000300950021-8
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• Document Page Count: 97
• Document Creation Date: December 29, 2016
• Sequence Number: 21
• Publication Date: December 31, 1972
• Content Type: ABSTRACTS

CALCULAI ItAN OF PLANE tkl-(;Tt4NSULA,-- VILATE-~S AM'-) C
Yl INI),',](.Ai ~-IMAA..S ON TM b AS I S (; F
VULIFLI;ViCit N A LANGUAGE-RU CUUNIRY-LJK
IZVEST. VSESUYUZ. NAUCH.-ISSLED. INST. GIDROT
EKHNIKI VOL 90 1969 89-101
FSIC-fil-23-2596-72

Transactions of the Vedeneev All.-Union Scientific
Research Institute of Wdraulic Engineering, 391 pp.
RUSSIAN., bk, Izvestiya, Vaesoyuznogo Bauchno-Issled-
ovate-11'skogo Instituta, Gidrotekh-aiki Imeni
B. X. Vedeneyeva, Vol 91, 1�979-.
Apr 72

Transactiom of the Vedeneev All-Union Scientific
Reseexch Institute of I~rdraullc Erwgrineerills, 423 PP.
MMSVM, bk, Izvestiva Y~esom?- Issledov.-
- zmogo Pauchr.0-
-4--'l 1~1-- 7--
APr 72

.... -, 1111-1111~1.1'1 "
-------- - - -- --
Experimental Studies of the "Orientation Effect" and
Deve1cpment of New Dynamometer D~signs for Measuring
Pressure in a Soil Mass, by G. Ye. Lazebnik, 17 PP.
IZVESTIYA VSESOYUZNOGO NAUCBNO-1.c)SLUDOVATELISKOGO
Instituta Gid ~t-ekhniki No 93, --.970, pp 200-20b.
AIR/.FTD7W-:'--2~- 9 5 0 - 7 9
Feb 73

Tranaactions of the
lReseexch Inntitute
RUSSM, jer, Izves
Vol 94, IM.
*NTIS TT 72-58oo4
B. E. Vedmeem, AII-Unicm Scienti:',ic _
of Hydraulic Imegincering.
. E. Vedeneeva
JU1Y 72

Tranmetions of the B. E. Vedemeav M-Union Scientific
Reserurch Institute of I~ydraulic Rngineering.
RUSSIM, per, lzyest~ya Vsesolu=n~,.,c Nnuch-4-no-Issledavat
L;-- .1
skoKia Instituta Gich-otekh7liki imiani R. E. VedeneeZa.,
,W~ ;P-~,
*11MIS TT ;M-58005
July 72

Transuctims of the B. E. Vedeneem A-U-Union ScientiTic
Researieb 3nstitute of Wdraulic 15',71-1rineer-ing.
RUESTM, per, Izvestiya Wesol= towo Nalichno-Issledovatel
.S) :~, 7-.-
Vol 96, lci7,l.
*rjTrs TT T2-58oo6
July 72

E. V. Burmakin
On Investigations of the Fishery Transformation
of Lakes by the Chemical Method.
RIESIAN, per, Vsesoyiizn-vi Natichno-Issledovatelskii
Institut Ozernogo i Rechnogo Rybnolzo Khozyaistva.
Izves i
Za, Vol 64, 1967, pp 5-17
NTO 72-12544-o6c
Sept 72

0. N. Bauer
The Study of Infectious Fish Diseases in the
USSR.
RLSSIAN, per, Vsesovuznyi NaLichno-Issledovatelskil
Inatitut Ozernoigo i Rechnogo Rybnolzo Khozyaistva.
Izvestiva, Vol 69, 1969, pp 5-12
NTC 72-12547-06C
Sept 72

DrAtci oil Lile Hj-):Lzc)oLol(-,L-z!, Dlcq
u _;jjoojr, w1(.1
of SiTliabludder Disease of the
carp, by N. 14. Arshanitsa.
RUSSIAN, per, VsesoyuzrKri !N-auc',-iio-Issiedo,.-a-uelsirii
Ilir'l-litilt,
1.4-vor't-Ya, Vol
J&al '173

llisLul.ot,,IcL~L ChwiL;cs in Lhe Livev, IULLnc~ s,
Skin L-aid Brain of Fich Sick Wit-11i lied liot,
K. A. FakLL)I10%,3.c1i.
RUWIta-, I?er, Vsesoyuznyi 11auchno-Issiedo-, ate-7 skii
111stitut Ozerno----o i Rec`.,.o.~o B,-,~bzno--o KhozI-.,-aist-%7a.
VLNI 63-101.
-n
Jan 7

DaLa oil the Species COulpusitl.021 wIld Ecc)lut~'
of Mold ~AinLd - Aj~ents of Saprolegiosis of
Fish oi~ the LcninLrad District, lb-~.- A. A. Floi-inskaya-
RussiAN, Per,
Insti-but Ozerno~,o i Rechno'-o IVonlo--o lZnozI-aistva.
IvIestaya Vol 01 U -123.
~), 1~1-1 ~), pp 1-03
WE -0"~c
37
Jan 75

Duta on the MiuloLV WILi Ej:)i'..OOtUIOLV Of Gill
Disease of the Carp, by A. M. Lop-akidna.
RUSSIAN, per, Vsesoyuzzl~,i
Institut Uzeriio-o i jj:,-bno,-o, Khozyaistva.
-- - - -' - - L~ -
Lwesidya, Vol U~' 1,A)9, -!?P 1224-130.
14TC
Jax, 7 3

"I"llo Propill-aLit)n t)i' Cull Im -c.,,~
Prom the Golludo of Fish b,! h. M. liubld-n.
.1 a
RUSSIA'I, per, Vsesoyumi:,~i Ilauchno-Issiedovatelskii
Ilistitat Ozcriioc,,o i RecluioL:-,o R.,ybno.-o Khoz.. aistva.
VL).l L,)~),
Jul 7

z' lfl.~ WI
On I'lomi, UC 111MILMILy In Fish, b~y
V. L. Vladimirov.
RUSSIAII, per, Vsesoyuzuyi
Instit-at OzernoL--o i Rec'mo-o !;Z~t)no-o
lzvostd')a %r()1 L-,,i I " -iL
to-OuC , P --, !~)P -13 '1 -
Jan '(3

Contrict Method of Deterinining Tomponiturer, i~ricl
nicrim 1 Fluxes Miriz-W, Grinklit.ir-1, by M. Shuttimov,
V. Sovkin.
RLOSIAIV, per, I~z~~~I:h UchebrWkh
7-ivedexiii No 2, 1,065, rr~ 17TUSI-0.
6 7548
Sci -
Aug 67 335,828

Conte-,ming the Theory on the Determination of
the Eurth*s Figure and Dimewsions by Satellito
Obsorvations, by A. A. Isotoir,
RUSSIAN, per,, Izvestiya Vysshy
idi Uchebnykh
Zavedej!y, No 3, 196S, pp 3-1-1. -9233226
RIC C;0962
Sci-Ear Sci
Oct 66 311,276

on the Theory of Determining -the Topographic
Surfacet of the Earth, by, 1. K, Monin.
llLkSSIANI* per# Zl=z VUZ No 6, 1965. pp 71-76.
ACIC TC-1172
Sci-Astranomy and Astrophys
Jun 67 327,310

I INA I i I I I I It H: V I A I I HIN Plel';~U~A--,, A ~., I I U, i~ if
aftWV&b*XcLj*atrlc'a 00nd,~Vjt3r a
5.Pp. ftmwl b-y M- A. ~'Tjwxw
,,-
Zdbar;jj-a'
~-Zvf% zmftuvn TAMIkh
ras 3-4 ---
WAR 190-' IV 2715-179. wjt
940o7aW
Bel 313j, 320
Xor awmarlog

~Y and
zis"s~Icii, YProslJOctilig by .!.;. j?. v
V ;
por, lzvos!_ 'Urato et al,
!Xa
)6(
Is I'll 3-4s.
I ~Zl 10
WL
Sci/li,?,rtil Sri
J~W 6 7
316,25s

Vie Optimwn Distribution of Load in a Power System
AtZowing for the Econontic Chaivcteristics of
Conownars, by V. M. Sinlkov.
RUSSIAN, par, Izvestiya VUZ. Ato 5, 1966,
pp 110-113.
0. A. Trans. 479
scilEzect
feb 71

"~lc 4*tO= Moloying Stmi for
M*Vm*to4VdroAVr*sl'* G*n&MtO3.'s, b3r 0. B. Bul.
F= GOVAWADIW LM a=
I-UBSZIWN.P pwi, -19vestim
AMM. NO 12p- R PP -1333-13-W.
&.6,23-1
Smv*nerg Omv
Bee 68 354P796

Solubility of Nitrogen in Iron-.Carbon Melts, by
A. G. Svy*azhin, G. M. Chursin, 6 pp.
RUSSIAN, per, Izvestiya VUZ., Vbl 12, No 5, 1969,
pp 43-46.
AIR/WD/MT-24-1418-71

r7VF,':-)TT.YA VY.(;r)IIIKH UCllEBNYKH Z11VFPrN.T.Y, AVIAT15IONNAYA
TKKflN.r,KA
COVER TO COVER
TRANSLATIONS BY ALLERTON PRESS

17,V VUZ, jIVIATSIONNAYA TEKHN.TKA, No 1, 1965, pp 1-169
Plitt tmawlaticn FTD-MT-65-72 P100029868-V

Bound=7 Layer on a Continuous !fAming PlAno
Sur;racAss, tar I, lo lbragimov & V, PO 1481*4rov$9 pp
AUSSIAI~, part AMAUM U Ikh Uchebaykh
j&v.*dw!&g Avlatedonnua- Takh Aa 2, jL965,
pp 18--p-5, FIGO102?68-V
FTD-Rr-23-M9-67
Sci/Aercm
June 68 359#315

Rqwdxmxtal and AnalyUjul ]Dak~~t:Lon of
th* BEG114n" Of RlWtla Tulftw Bearlnggs by
Yee A. Art4mv.
NMOXANV s Uv VUZ AvUt INgh. Vol 8j* No 21,
2965j, vp m5l~.
RLV-69-19985~431
8"44wlh
Sept 6c.) 391j,253

iiacict w, trio TJicrj:.ody-jjaz-d.c Proll-u-i-riw; cif
thu .1 On U-0-- UJOLZO 01'
q)tiuumi Parameters for a (L-iss Turbine,
by U. N. Yemanp N. N, 6ykov.
116SIM, por, Izv IfUZ Avints Tokh, No 2,
1965. PI) 65-75.
NASA Tr F-335
Sci-Fuels
Jail 66 294,529

,j2 a
WJ-1Xtichargo Sourceg; of :EOMB. find Atoms wit
GlOwll2g- Cathodep by 0. V. Ko:aov and YU.A. Aablo,
ct al.,
RU3S=,p per., Imeati3m K& AvlatsLsegm Tekh-
No 2* 1965., pp 67-91. F100006767
sai-Nuel scl
ftb 67 33-8,349

,%z AsymVtotIc ftt-hod for CcmPutima the Teimper-
&turn Field of Ciao Turbim Movina Bla up
by I- So Iqubehedwo 14 pp
RMIAN, Verv bm"-w-ug-a-1p3raisbAkh Reets1h.
FM22VAT- Aviatsdampag Mokbmlka* Ito 2v
1965, IV 92-Im- PlOD1203W-T
rv)-itr-67-ho
fti.Propj]Alm and Puels
jay 68 350oftl

'ilh-- Oiisuipticja and Pxusstwa- aiarac-Wxisticz of
~l ix-O"It.) Tuxlpojot i-~I'jilx) "'ixin(.) aliwix-Ir, Irl
Ye. D. Jttml"i. 8 pl.).
RUiSLM , per, Izvestiya :Vysshim- I uciidxiy]J-l
ZZIW4 AviTUI'Ciulaya Tektuiika No 2, 1965,
op lj-5-j2u.
jUIV17TD/Ifl'--23-1656-67
sci/prq:)ulsicn and fmls
mar 69 377,824

I~,'Iition Cc4lditiull '-on.-Tiler-lal Activatio;.
w* * a I:uol i-lixture, by j~. (". 1"hudem-Zo.
1
por, Iz vtlz, Avlat Tuthil. 1.-0
1965, pp 121-131.
Dqpt of Navy 4524/,WL/,r,113 T-1662
Sci - Puals/Prop
f4ar 66 297,793

Additional Energy Losses in Cooled Gas--Turbine
Powerplmts aid their Influence on Specific
Cycle Parameters,, by R. G. Khairullin aid
V. I. Lakai.
IdJSSIAN, per, Izvestiya VySshikh Ucheb5~hh
Zavedenii., AviatsfonaEya Tekhnika Vol d.,
No 2, 1965, pp 152-158-
NTO 71-14239-13G
~L,Z-Scx, -rT-
Feb 72

Visualization of Transition Phcmo=na in the
4oundwry Layer on the Bladej; of a Turbine
Cascade, by A. Ya. Ipatonko and A. M. Antonov,
RUSSIAN, per, Izvestiya VU-Z, Aviatsionnaya
Tekhnika No 3, 1965, pp 76.!82. P1055USK7
MD-h - -319
Sci-Enorgy Conversion
Feb 67
318.949

Surface Ionization in a Porous VT'all, by
Kh. V. Kesayev.
RUSSIAN, por, lzvostlya VUZ Aviat3 Takh,
No 3, 1965, pp 937-08.
FTD - S - 4*99 (, - (,09
Mar 68 378,624

Dotermining the Temperatuxe Field of
Turbine blados wit% Longitudinal Air
Cooling an the Basis of Asynptotic
Mothods of Analysis, by 1. S. Lyubchanko.
RUSSIAN, per, Izvestiya vxsshikh Uchebnykh
Zavedeniy Aviatsionnaya Tekhnika No 3,
T963-. pp 88-107.
ATO 66-51
Sci-Phys
Jul 66 306,490

A, Tiklivrdrovp IU lys
IUBSIM, por, Iz YZ ssli Urliab Zaved,,
I INO So 19U5, p'$ IUS-118.
wiat Wful, A!
DC-39011
Irf L~-W-65-1656
Sci - Engr
Jin 66
294,736

Finite
ic o J:
t'ho PrWiLl'.-i oi: [lout Trwustur
UIL:~ and Turbinu Blade, lif A. Topulov,
Yu. N. Kulesh, 12 pp.
RMSINI, per. Iz wssil U:Iicb Zaved,
Aviat Tokii, Jo 3, 1965, A) 119-12o.
1'l 6 U 1-4-116-6
FTD-HT-66-487
j ci - Phys
J.ui 67
317.643

Det-anAnation of tho CombuffUan Chambor Lmgth
kloccamary for complato I-Aiol C;ombuBUon laldng
Xcto Aooount Friction of Gas Flow During Its
kvbion # tar V 9 V . LVdwov pp o
RESSUM, per, Izvggga Uc
Wx2dSAY 2 Tckg-~. No .3, 3.965.
pp 127-130.
ADqf TI),IIT-23-1355-67
Scl-Prop and vuela
nov 68 353,690

T,Dstz with Stagnation-Terpeimture Sensors
Having an Internal Channel by the Equivalent
Pressure Drop Method, by B. C. Vinogradov,
bf. D. Yermolayev.
RUSSIM, per, Izv VUZ Aviat*21bkh.No 3,
196S. pp 157-162.
NASA Tr P-10.041
Sci-Aero
Jun 66 302,034

The Teurporature Field in 3n Infinite Plate
Ileated Simultaneously by Radiation and Convection,
by Yis., V. Vidin, V. V. IvanOV.
RUSSIAN, per. Izv*VUZ Aviats. Tekh. No 4, 196S,
pp 3-6.
NZSA TT F-10,960
Sci-Phys
Jul 67 332,900

Oiu.,.ic Proportias of Liquid 1:.Lcx,: 'llirough
~~-'paccs tioasured in I'licrons, by G. A.
Plikitin.
I'lKiSIM, por, Izvostiza VUZ Av4atsicuinaya
ToMmika, No 4-s-IM, pp 38-45.
AG i1 J-1342
11) 22U4OS8666
sci-phys
Fob 67 317,741

A Thin Profile of a Bupersonic Wing vith
MrAmw Average Beat Transfer CoWleleat at
Gives Aerodynamic Characteristics, by M. B.
Polyakov and Ya. S. Shchei-bak, 14 pp.
RUSSM, per, IMMetlya I)Mahikh 106%
EaWIWA- A451612SM -T-10~)'
VP 51-61. FICK)3M9b7
I'TD-HT-"-491
84-i-Aerovautics
Do a 667 344,431

DotenduatIm of CartAn Geemotric Parmatera of
TUN&* GrIds. bW B. M. Avenmr, 23L yp.
mmue PWO I a -
Umi"Arl- Tw- a so 4, W5,
e F=3?"67
WVM092"s
Salow & Fiala
im 68
3W.649

IUT**t of the *jxfber ot Rotor Mad a an
the CharacUrisfAce of an Aziradial Com-
promeor,, ty A. Me Shmstyukp Yee N.
Zayobmkov U Ipp.
MOMMOR per* Imun Exubm MW
"M
Zgwadal&T. Aj[&%t~lqmjM, Tokbnikw no 4,,
1965p pp 125-1X.
PIOMM720
FM-Rr-"-769
Sol-Aaroppme Ul
74ib 68 350.,6W

cu L It ILI' I o j:
1 IV . V(;Z. AV i.1 T(4A I.. .-:o
EMS, J."o 103-109.
AL C- K- t 1- 11 .
Sc;/Enam~,.y Conversion
,Al.ir 67

IZV-E-TI-YA VUZ, AVIATSIONNAYA TEKHNM
(Soviet Aeronautics - quitrterly)
Trarinlation begins with 1966,
Vul. 9, No. I
Order from., The Faraday Press, Inc.
B4 Fifth Avenue
New York, N.Y. 10011
1971: t 125.00/year IT-QA and Canada
t 130.00/vear elsewhere
'k 40.00 single is-~ues
Price of back volumes! t 125-00/year

Ilypersonic Gas Flow Around Conical Bodies,
by 14. M. Monakhov.
RUSSIAN, per Izv VUZ Aviats Tekh, No 1,
1966, pp 3-11./5-
Dept of Navy APL/JIIU T-2256
Sci-Phys
May 69 380,950

Trin Chartwtoriatics or Supmraorde Aircraft,
by S. Yu. Glcripnichenko, 17 pp.
RUSSIAN# per, Izve6tLYa lashikh lUchebnYkh
Zavsin-i-z* Aviatsiomaya Tekhnikav No 1.
113i%, pj) 16-27 - P100339767
FTD-nT-66-7&3
Sci-Aaronautics 346,454
jan 68

Stabdlity and Natuzal VWjmt&cvw of Trunmted
AructtiTAIly~-(Tthotr*p&c Cmi(al shnUv,tor
V. F. V4tuabldne A. N. KiMgWmko.
.d-
Au9sim"I Part lam#Aa !Dmas M ubhebraich..g~vv
g%y. AvlatgLqmwe T'. N --3:9-66~- PP 73-
79* FlOM24168-V
1i-TD-IV--24.aA-67
SCKL-Pkvs
ita 68
359,891

Praw4ftwom In jemUM Grooven of iiydraulle Amow,
b3J.es,l by P. i. wAridov,
RUSS=-1, per, Isyg#.j
,1! y0shUch Uchgbnyktt
Zavedenty, Teld=ika. No 1,
IT 90-994
Jul 6B
359.892

Instability Criterion of a Developed Deflag-
ration and the Analogy Between Combustion Pro-
cesses in a Detonation Wave and a Rocket
Motor, by So K. Aslanovp
RUSSIAN, per Izv,, VUZ Aviatsionnaya Takhnika,
Vol IX, No 1: 1966; pp 10-37114*
Dept of Navy/AZL MU T-2018
Sci-Prop & Fuels
Aug 67 333,0S2

Convoction Jloat EXO=go in a (,'Io:;ed 6pace
Betweerk Two )~Otating, Disics Undor Turbulent Con-
ditions '~Iowp by V. 1-1, Yapinas.
RLWIAR, per, Tvvwti
-va VyssIdkh Lblobi j
--- _1-
?Avecl,or!~yt.._.Aviatsionna5,pt TaWmUm, 1966, -hel
12 9 iS 16 -6 ffL d K,
Jul ~s
359,893

91oiei--iAi V, /I
Certain Problems of Gas Dynamics of Stremms in
Transverse Flow During Burning, 11 pp.
RUSSIAN, per, Izvest3.ya Vxsshikh Uchebnykh
Zavedeniy. Avi-atsionnaya Tekhnika, no 1, 1966.
pp 130-139. P100081568-V
FTD-MT-24-303-67
sci-aeron
may 68 356,378

11so of Dorivntions or Thenral 1(~nition Theory
to D,,4torndae the General Flame Stabilization
Condition with a Bluff Body-, by V.A. Mironenko,
a pp.
HUSSM, per,, Izveatiya-yyashikh Ucheba;2Lh
Zaveden~44. Aviatsionnaya TekhnikEL No l.. 1966,
pp 140-145-
AIR/FTD/HT-23-lo66-67
Sci-Propulsion & Fuels
Nov 68 3660275

Separat ion low Around a
Vibrating
RUSSIAN, 3er, Izv VUZ. Avia-toionnava Tckhnika
1966, no T, pp-rq-g,-=S* FIUU124lb8-V
rTD-MT-24-131-67
sci-phys
jul 68
Profile
35911894

Maintaining Flow 81-41arfty In Calibrating
Nozzlea Used in Stu4ying the Working Pro-
ceases In PmVs, by 11. S. Yershov, jo pp.
MMMI,, per, Izv VUZ Avlats Te!g!l Vol 9,
no I# 3,966jp
AM/iTli/~fr--2~;1224-68
Sai-Mech
Nov 69 L395,894

Yermolenko S. D.
Nonlinear Theory of Wings With Small Aspect
Ratios, 15 pp.
RUSSIAN, per, Izv VUZ. Aviatsionnaya tekhnika,
no 2, 1966, pp 9-18
P100208868-V
FTD-HT-67-177
NASA PP F 10,915
sci/aero
sep 68 364,210

Stability of a Cylindrical Shell With
Elastic Filler Linder External Hadlul
11xv3sure, by B. A. Korbut, S. G. Saksonov,
6 pp.
RUSSIAN, per, Iz VZsch 11cheb Zaved,
Avist Tekh, No 2, 1966, pp 38-43.
CMFDD X-5910
Sci. - Phys
Aug 66
MR OFFiaAL um oNLY
:50S,6S3

The Probtlem of the Innuence &MIrted bY the
ftleame of Coalina Air frm IU MAMis into tha
Flow Tkwough Portion of a Gass 'Watdne an the
EMc4wncW of the Latterv t7 To. 11. Bogm01OV,
1.5 PP -
AUSSXAII* per* 1-saf-ma
0
Ll~ No 2j 1966t
m ~ Twd
pp 49-3B, PLOD187268-V
M-HT-67-303
Sol/prop & F1019
Sept 68

calculating t~i-- iweakdan Caiditiaws of Cax-:~-
hu3ti,:n in the Idw belLind a. Bluff I'Xicky by b-le
IA~Jay lk-iriod of lLgxit;iai, by V. .1. tlraw--nka,
8 LAp.
IISSI-ALIJ, Per, Iz a Mrsshikdi I!L~i~
Zavad!!I~X. Aviatsicnnaya 'IL*hnika, No 2, 1966,
pj..) b&-73.
ILI !VI-TD/'I,-q--2 4-134-6 8
sci/produlsion and fmls
--n-r W)

.,o of Tvo Gas !~loivrs
conow-ront I)isallarr
Through a Jet ITozzle,, by
Ya. D. StenlIcin, 10 pp.
MUSSIANI, Pero lzvest~ya asshikh
'Uchob Ch -.,.CLvaWO-nfY-. AVirLtSiGMrl,-,Z
TPoldirtikn , . ' 83-89-
P1002061368-V
F."LD-E&T-67-177
,qci/?roP/!Alcls 364,211
sen 68

Doramatlon of Axon of Par&ULel Stz*wm During
Tlm:lr Inte"Jectlon, by B. Ga Xhadanko, 14 pp.
RUSSIAJI0pwo IM, Avial m WO T Lkalp
Mo 2* 1966, pp 90-99. 1?10015666B-V
FTD-M,-67--oo
Sai/FIWB
Sept 68 364.959

itlyaxzonlc k-rofile Of
Having an AssiSwd Banding Strangthj by,
Yo. Ar. BalySim, YU. N. YucUntoov.
Vz S*r LnIss - TbWm
IIWJ,MXj, per.. &V Av. =
So 2.0 1966., pp 119-12.5.
NASA TT P610j, 639
sai-pt7s
ikr 67 33-8,735

lUiz:- calil3ratim of
11-L'AlAllellt-G. ill Di~jitill LXx;llljW-X-s, -1),,
;' 1. t. Golovin, A- P. Tui-&ui. 6 pp.
IzUZUA-4, ixar, va Va!;Iiikil Udleinyidl
zavmjl~miyl livi-a M-amayaTeiamaka, No 2, 1966,
1--)p 12(v-129.
AhVIVDIRP-2 4-134-6 8
sci/c,lectmXic~.
mar 69 376,559

ExIxtri ntal Investigution of the Influence
of ThermodynWic Properties of Liquid an
Cavitation Phe na, by N. S. Yershmr,
B. I. BDrovskiyp 3.1 pp.
MMIM,, per, lzveLtin Vymsbikh
Zawdenly. Aviatslonnaya Z*hnika No 2, 1966,
pp 130-136.
P100014768
FTD-MT-67-40
Sal-Physics,
Fab ba 350,625

ol' Cuti Jot5 at a by L. A. 7~ml'ova
sand 1. ). ;lAuruv, ot al,
IWSI/N, par, Izvostiza VUZ, Aviatsiva Toldai.,
I -
No 2, 1,.", pp 137-142,
Dopt of Navy 5074/APL 1948
Sci-PL>s
Doc Us 3.15,537

M*Vt-am for Optimum Dwdgn of a System of Shocks
In AxiAlly symetric&l supers(mlo Diffuse= with
hwb~l Compression, by A, Po l>adovcVav* 4 ppe
RUSSIAN, part IsveatiYa YngN..kh RLhqbW!$t
Zovedenly A!j~~ lLklL. NO 2, 1
Pp 153-133. P100046665--v
M.ur-23-682-67
4F5 -3
Ekw
Apr 68

CAI-culfi.tim of the Angles Of 'Dmrmvh of Elovy
kUftnd RwtwWxUr WInge of Sim2l Aspoct Rmtjo at
S~ksonI.c VGI*Oit:LGO AOCMdi~ to lion-Linear Theory-,
by S. D. &uclankos 1-1. T. Barinov*
RUSSIMI, Per* U&.,VUZ Aviatsjek
pp -1paos A, No 3, 1966.
NLL Ref s 5207 (2247)
j PPS -S -1 /Cr-~
SOL-141IFS
Amg 68
361.692

Calculation of Laminar Friction and Beat
Rolease Characteristics of Ifigh-f-empern-
ture Gas, by 1. 1. Su*sov.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 3,
1966, pp 23-33.
Dept of Navy APL/JRU T-2261
Sci-Phys
May 69 380,955

Idtz Method in Nonconservative Proble m.
of Elastic Stability Theory. by
Go A* Murchanko. 6 lip.
RUSSIAN, par, Iz Vysch Uchub Zaved,
Avint Tekh, No-77-066, pp 62-68.
CMFDD X,,; 000
S ci - Phys
Doc 66
USIB Internal Nuse Only
314,181

Crvwrion of the ImtabUIV of an Arbitrary
Systen or Def3AkgmtJLon In the Combustion
Chwftw of a Rocket Mmal vIth Successive
Aut(dodtAon of the Fuel, 'by S. K. Aslanov,
4 w.
yeablikh
BOOM,, per, Izvestlya- V
ZavfKleniy. AVUU12~ I No 3,
TX5,, w 85-W.
Piwmow-v
Pm4m-e3-1047-67
Sal.-Propulaian and Fuels 366,152
Oct 68

Tho .211oleoular llimint.; V01001ty Along
the Basio 3ogmant of a Illurbulont Jot,
by A. G. llradnilcov, N. A. 'Zamyatina,
IRUSSIAN, nor, Izvastiml 1.17sabil I
'Uchab ch "alirozonly. iliriatsiorma7a
LIZ]
ilo 3, 1966, m) 104-1:LU-
.100204U68-v
-r,,"-67-212
Sci-FrOp/f.*ucls _3 6L., 17 3
-Sep 68

Towards and Appraisal of the Influence of'
a Cloziranca outwot)1i tho ".1ing anf the rlar)
on the Carrying Characteristics of a Pro-
file with Blowing on the Flap, by
A, 1. Matyazh.
RUSSIAN, per, Izvestiya VUZ Aviatsionnaya
Tekhnika , No 3, 1966, pp 120-124.
FTD- S -72-41Y _2 / -/ - & ?I
Jan 69 374,180

Sffect of Degree of Admission on the Forformance
of a Contripotal Turbine, by A. le, Ovalevalcaya,
RUSSIA.ii, par, Izvostl3e &ss*~Jkh Uchebriykh
ZavedwiLy. Aviatsionnaya .1elchailm. No 3. 1966.
pp 141-148* PIOO10466?,V
F-M-11-T-235-M-67
Sci/prop a- I-evels
June 66 -.1 --359-pqp-~ .'~ _. 1- . .. .-

(~)Lilial "I'lAbilizatical of cou~~tta by
T. K. txIblov. 8 )A>.
lal.;'113IM, ',A3r, Izves4ya 'vN--sl i Ud-xlmykil
Zavadmiy. Aviatsicnnapa TFJ-duLika No 4, 1966,
pp 23-28,
Al IV1-TDA a%-2 3-9 19-6 8
sci/iAlysics
nW 69 381,193

Free and Parametric Vibrations of an
Infinite Cylindrical Shell in an Acoustic
Modium, by M. A. 119gamov, it. Z. Kamalov, 9 1)1).
IWSSIAN, per, Iz Ak Nauk Vysch Ucbeb ZaveL-
Aviat Tekh NO-Z;M966. pp '11-50.
CIA/M 079
Sci - Phys
Feb 67
FOR OFFICIAL USE UNLY
317,697

An ApproXiMate Method for CalculatLni, the
Parmwatore of a Detached Bow Wave, by
Yu.I. Klimnyuk and A.P. Kmarov, 13 pp.
RUSSIAN, journal* Izvestifa V-ysshikh
Uc1iatMXkh Zgvedeni-y- Avi tsionnaya- Takhnika,
No. 4, 1966, pp. 81-89. T100006468
FMAT-23-837-67
Sci/Acronautics
AuE, 67 351,543

"-u-,r,4y 'era-wter Li Cumtrlll,.~,al aia
i~txijki by Cixculaticai zuicl Coxioli~;
1A),rmi, by B. V. Ovzyauiikov, 13. :1. Boravs-kiy.
9 pp.
IWSIM, per, Izves4ya yys:aliikh Lbli,-ImykJi
Za%ucblli Z- Md3[=:.cqnaya viika, Wo 4, 1966,
PL-) JLU7-113.
AIPAVDAUL-23-683-68
sci/enarx
.1y oanversi(m
apr 69 377,946

Optimum Conditions of St4)cvouic Flows
With Oblique Shock Wavas anti Subsequout
Heat Addition, by V. 1. Pensan, 10 pp.
RUSSIAN, per, Iz VUZ Aviatsionnaya
Tekhnika.'Nu 4, 19M, pp 11AM20.
FrD JIT 67-26
Phys
Jklay 67 xM4,961

Flight Regims of a Vehicle With a Ramjet
Engine Whicli 11rovide for Cons.tant Conditions
of Fla= Stabilization. by V. N. Gruzdav.
A* V. Talantov, 13 pp.
RUSSIAN, per,, Iz VUZ Aviatsimn!xa Tekhnik-a.
No 4, 1966. ~P- 17V 8. PIU01846b7
VrD IIT 67-24
Sci-Prop and Fuel
Jul 67 331, 437

Uso of Uombined Coatings In Radiation Ecating of
MAnks q by I. A. Zernov , 7 pp.
M Vysshikh 11che
RUSSIM, per, I:zve#.i bnyidi
& nika
ZavedmLy. IE~&tsloMvaya Tekh Vol 9, No 4,
1966, pp 136-141.
AIRAfDAT-23-M96-67 AD 0'79 7-36
Sa-Flech
Feb 69 X/2,974

Deter -inaticn of the Ocst oj~ an Airax-a-C-t as a
FU-icticri of .-k--litfiit and I&ag- of the CUder Wits,
by A. A. E,'Wzueatsov. 10 pp.
IW'61IV4, JA31r, IZVr--S ja \~Ysa"l udvatxl~Nl
V.-tvku. Av =ats ainaya IllAdmika, Mo 1, 1967,
pd 3-9.
.,U IVM/16 111-24-210-68
sci/bWiaviori,d sci
may 69 381,170

Scuo l.-'roblear, of tlic Structural ",txongth af.-
Aircr, 'ift, by 1. F. (1,mizLsov. 14 pp.
1(W11144, Lx-r, Izves va vyqsllikJi Uct"xiykil
Zavadmiyo liZatsimnaya UL-kimika .1967,
pp 31-40.
AllVr-llU/irD-23-1663-67
sci/aaxcnautics
apr 6 9 377,941

SttEbility of an i'qiis(*-m,)ic CIrcular Cylindrical
--ioU un(br ):nWnlill
by V. V. Ifusbalov. 11 lip.
per, Izves ya ~Z~iikh Wielxiyldl
ZmedmAy. AZ~a-tsi ava WUuilka No 1, 3.967,
p1? 37-44.
AtIVIvll)/j~U%-24-210-68
sci/physics
jyW 69 381,160

StcacV-State Radiative float 'Enwafer Through
a 13mied3wface with Variable Thermal
Canduativity of the Material, IV No P. Belik,
Do A* Kcau-svp 4 ppe
RUSSIAN, par# Imm Vysshikh Uchabrovkh
Uvederd Avlatsionnom TokhnUm, no it
1967~ pp 61-64.
AIR/JFTN/Etr-23-1334-67
Sci-ftys
Jan 69 370,803

The Fousibility of Dosigning a Uniform
Strength Blado ou an Air Cooled U.'sicasod
Type, by A. G. Zenukov.
RUSSIAN, per, Izv VUZ Aviat Tekh, No 1,
1967, pp 107-113.
FTD-S-FrH ,~6 io-~,q
Apr 69 380.ftt 662

rilow-Rato wid YereswAre Coofficients on the
surfaw of a Cmdeal ~Iow at JIMMrsonlo Velocititiap
by A. 141, kfthitaryan & M. P. (mrjwirdkov,
RUSSIAN, per VUZ IEv., Avis;taiorma-w Tekhoo
Vol 10, No 1: TIW"o pp 125-12.7s
Dept of li&vy/APL/JIIU TG 230-T.541
Sci/Phys
Apr 68 35io238

I'low FIDId BeUmen a Shook W"ave and the Laterai
Surfaco of a Blunt Com Floving at a ai& super-
00nic &jp"dp by E. R. Aborawrakii.
RUSSIA11, por, VUZm 1xv.. Aviatsionpa-Nm Takhniks,
No 1 t 1967 s 1 420
Dapt of -1 JHU T-2098
sci/p1w..,
kkr 68 350,990

Vibrat-.'Ion of a Cyclindrical Shell Under
High-Frequency Pulsations of Internal
Pressuirc, by Sh. U. Galiyav,
M. A. 111gamov.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 2,
1967, pp SO-57.
AIR/FTD/MT-24-14-68
Sci-Phys
Apr 69 379,530

Bending Analysis of a Tlij; 6ii-Walled Structure
Taking Short-Term Creep of the klatOTial
Into Account, by S. S. Krestovskiy.
RUSSIAN, per, Izv VUZ Aviat Tekh, No 2,
1967, pp S8-66.
Dept of Navy APL/JHU T-2232
Sci-Aero
Mar 69 376,242

Exporimental Investigation of tho Inter-
action Zono Suring the Injection of a
Socondary J6t into a Plane Supersonic
Flow) by B. S. Vinogradov,
Z. G. Shaykhutdinov.
RUSSIAN, per, Izv VUZ Aviats Tekh, No 2,
1967, pl) 81-88.
AIR/FTD/MT-24-14-68
/7 PL- /,~- H (, t 7--
Sci-Phys
Apr 69 379,539

Design of Optimal Controls in Linear 'T%io-
channel cross-Coupled Systems, by
Yu. V. Alcksandrov.
RUSSIAN, per, Izvestiya VUZ Aviatsionnaya
Tekhnika . No 3, 19 6 7, pFl:t~~. / - / cl
FTD-S-2&33 - 6
Jan 69 374,182

Application of the Concept of Engineering
Stability to the Problem of the Longitud-
inal Motion of an Aircraft in a Turbulent
Atmosphere, by Yu. A. Val.'kov.
RUSSIAN, per, Izv VUZ Aviatsionnaya Tekh-,
No 3, 1967, pp 20-28.
PTD-S-3" -Z:~ 3 - ( , X'
Jan 69 373,280

Determining the Field of Temperatures in a
Transverse Section of an Air Cooled Blade,
by A. G. Zenukov.
RUSSIAN, per, Izv VUZ Avisitsionnaya Tekh,
No 3, 1967, pp 52-60, 117-124.
FTD-S-46* /s--s- (, )
Apr 69 379,516

I
r.-c'Rict 01 11-10cx.Phate. CAI Lao !.-:ffiaU--II(:y
of a Jypits~3 Tuifiojo-t by Yo. 1). -ton'Um.
11 Lit).
UNSLU, por, Izve,,- va Vysshikh Uciiclmvk-li
Zr-AVe(I?JIiy, A%Ta-t-s"i"amiaya Tbkluuka No 3, 1967,
pp -75-W..
AIIVI:TD/Ml~-24-300-68
sci/p.tq)tLIsicn a-id fuels
nW 69 381,202

-,-'lZL
'CC! Stabilit-I O[jTIlCdtil-,flf3 Ll -",Y0f'V3S DucL
OcxbmLlcm
by ;~. V. -xitialtov, V. 1j. L;ruzLi-!V. 9 13p.
VWSLNIJ, per, Izvas!AXa Ni-y,.sshikh Uchebnykh
ZT!~~' . AVi=tploMaya ~~a' NO 3, 1-967,
pp W-880
AIlVI-7TD/r.ll%-24-30D-68
sci/prcpulsiczl aid fluels
rmy 69 381,,203