FR:INZHENERNYY S. TO:INZH F.Z.

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• Publication Date: December 31, 1983
• Content Type: ABSTRACTS

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D-SIR LLU (10M) M, 740
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63-17473
Meldunam, L L
AN DMEhMQATION OF THE PROCESS OF VIBRA- 1. Mokh=4 L L
nONAL DRIVIM OF PILES AND MEET PILE& 11. A'M-QNOR
M. Associated Technical
Orft frMl An $17.73 Services, Inc., East
Ornoge. N.
117i~ o( Akalomiyal Nauk SSS& tut
19K V. 19,
P. 00-01.
DESCRIPTORS: *Civil en&mrifl& Cm9ructiou. Vl-
botim *BMW (Suucuml~ Shme, MW pum,
Foundaims (SUV=M)
(Eugneering-avil. TT. v. M .1 udww S.Mm

sf ttc rreep of Tarti=
Diacs, by V. I. Rozcnbly=.
RUSSIAN., per.._-LmzhenerW Sbornikp Vol XXP 1954,
pp 49-54.
DsTR LLu m.965
(loan)
Sci - SW -
Oct 60 / ,2 g)p ~'

An Investlg%tion into ftvitational Erosion
of HI&-Pover Turbines and Pumps,, by K. K.
BW 'nev,, 35 PP.
RUSSIAN, per,, ln2he!~qnuf4. S.bv,n,lkl Vol
xvin" 1954., YfAd.
Scl Mus Lib 55/3409
Sci - Engineering

Caicuiation of the Creep of Higb-Pressure
Turbine Discs, by V. 1. Rozenblyum,, 11 pp.
RIMIAN, per, lnzhhenergy Sbornik, Vol XXI
1954, pp 49-54.
SLA 6o-i3.63,,-%
Sci
Vol IV ~ NO 7
Apr 62

On the StablUty of a CUsed Two-laywed Conical
SM32,9 SubjeoW to VWam Nmul Pmemre~ by 3.
Griplyak, 25 pp.
RMUS9 pWj Invi"BrIWL MMWAkv X*29p 2954p pp 73-
&d Tr C4WtW
AT - 3645
J7
Avg 1956

M,bj, d Abstracts.
7 , of contents r-~n
;,,USSL' " 1)(21 Inzb~.,nernYi Sbcxnil~, vol ,,-x, 19)" ,
-:1 .1 1).
I
1- f,~ . 'Encl to LI-1751-55. CI~, D 3h300"
) ~
1
699793

calcmiation of the Creep of Higb-Precaure
Discal by V. 1. Rozonblrtmy 11 pp.
RUBSTAN, Or, X=berermy Obornik, Vol XK,
.......................
19542 :pp f.9-:~4.
sm 6o-i3839
Bel
Vol XV;. No 7
Air 62

BlidlOg Of CU%MIW aOd RUW-WAMW PJAOG Of
Taying or unuum skukoe" Bayod the mostf
LWI# by A. S. &ISM7WO 60 pp.
imms p"s *be~ Sbomik VOL U,
pp W-W.
ftl as ub no 0/mg
scl ph"Ics

&thematico-Statistical Deacription of Surfaco
Profile irregularity In Grinding,, by Yu. V. Llnnlk~
at al.
RUSSL45,, per, Inzheraornyi Sbornik, Vol XXO 1954;
pp 154-159, amq'
Co-op Tr Sch Tr 367
Scl - blogr 4 L~
Mar 58

T~,ble of Contents end Abstracts, 12 pp.
I
Eussiil-,N, pA-,r, Inzhc-nernyi Sbornik, Vol XXI, 1955.
Encl to L-~-1751-55- CT-J% D 3~3008-
AF 69970/---

Tbrsion of a Circul.-.,J- Cylinftr RainfUrcad
Vith an ILliptical Rod, by D. 1. Mama.
RMrAN.. Ver, rMAmerftl MmTlk.,
Vol Wi 1955) li~ 79-9b--
camo
act - ftv
/W '-rdr~/
*r 62

Applicatloa 01" Vlic Njtbcd of A. F. 1.czo"-2:.a
to tho Calculation of Eunmr MudeB of Swivo),
Made Watcz Turbines With the Detmination of tho
Cacfficicmt of Cavitation; by 1, B. EtlnbarGh..
28 pp.
PIUSOM111, per., Imbenernyl Sbornit Vol XXIII
1V~5j pp 163- * 6~ 8 ~
sci ma Lib no 56/2234
Sci --Dnineering If .57
1

on the Appl4cation of ths Xet4lod of B. 0.
Galeftlo to Uwar Pralow Arising 7m
Dymacal Dys+Am With DlatribvW Paramou",, by
a. 0, Our*debp 10 pp.
RMIM9 parp babooMi ftanftp Vol 10=e 1955p
pp W-52.
ABC AM Tr 372
Sci - Pbre
Sep 58 7-Y, 7 9,.y

Diftet M42" of 8(klvb* DwjWW Tabw Problem#
bY A4 Filins
A
-AMU# Very Indwn-qmmLMwm*s..VOI M=#
pp 1055,-t-
Md*f Ubwerteas 09091aloO,
3A AUmwt Otm
X"It NelbWaMp AUSUSIft
0. 2,. Ra.
Bel
*p 6o

Yrrvec.t4pntion of the Stability.of ribin Envelown
Uith the tJ.d of 114aer Models., by V. M. Chebanon.
RUSSIAH,, per, _Inzh ,TLqLSbqrnik , 195-;?
,,j Vol xxii.
PP 150 -159.
C. 0 I.R. 0.
Sci
may 60

Some Cases of the Elastic Equilibrium of an
Anisotropic Plate With a Noncircular Opening
(Plane Problem), by S. G. Lek-linitskiy. 37 pp
RUSSIAN, per, Inzhenernyy Sbornik, Vol 22, 1955
pp 160-197.
Al R/FFD/fIT-2 3- 366-69
sci/mechan engr
mar 70 404,392

Finite Deformation$ in the Fare Bending of
t;,. Rectangdar Strip, by L, As Thlokondkov.
I
RUSSIM, p~r, Xwhemwmyl Sbornik, Vol xn,
1955, PP 18,3-M-
Sci - Engr
Jul 62 ,.-4 -/,

GtabUitY of a Cylindriftl Mel". Wlth Trawvame
Stiffening Under ZxtAv-,-" UnUorm Pmasure, by
17. A, Allfutar pp.
RMLO, per, mmrsilk, Vol MMIp 1956j.
pp 36-46. CIA-- 3
Aasn Tr No 1026

meeT. cf amp va tAm DistrIbution of Interwl
Strasses Is Orftotv*ie Molls# by I. E.
Pracparich. ussvm
MMYAVp $or# Imb,09m;ks va MWO 1956o
Pq 151-i&# ""' - "' -,
Sol - fts
out ~a 76~

T7' 7Ti '77
Comles" Bari, by A. N.
no
9IT-921*
AABC SCL.T-6&252
rap&"
i= 6T

On Some (~iadrstuns of Fimdamental Beam
Functioas, by R, Do Stapanovs 6 pp,
RUSSIAN, per, Inghen Sboraik, Vol XXVI,
l9ss" pp 94-10F.~
CIA/FDD X-5889
sci - Phys
Jul 66
FoR oFFiaAL USE CINLY
305,p632

Stepanov, R. D.
ON THE FLUTTER OF CYLINDRICAL PANELS.
MOVING IN A GAS. 119621 [151p. 3 refs.
Free copies available from Boeing Scientific Research
Labs. Library as Boeing Trans. R44. When supply Is
exhausted, order from OTS or SLA $1.60, 62-18855
62-18&55
1. Stepanov, R. D.
It. Boeing Trans-R44
Ill. Boeing Scientific Research
Labs., Seattle, Wash.
(LAka Nauk SSSR. lqgjUz-Mckhu01.
Traos.-9
oL~-'- _j~ 1959, v.2F. p. 92-100.
ne~nyi tr~nik.
lnrp --- -
k
DESCRIPTOR& *Aerodynamic contigurations. OPanele
(Structural), Cylindrical bodies. *Flutter, Supersonic
characteristics, Stability, Numerical analysis, Complex
numbers.
'Mis paper gives an application of a method to the so[
be flutter of a circular cylindr
tion of the problem of t Ical
&bell of hollow sectio& moving It, a gas with superwnlc
velocity. It Is assumed that the shell has hinged fasten-
ings at its longitudinal and transverse bourocUng edgesu- oft of Tothmkw SWV*U
(Mechanics- -Aerodynamics, Tr, v. 9, no. 4) (over)

One-Dimonsional Problem of Temperature
Streases In an SlutopImUc Medium, by
V. A. Lomakin, 3 PP
per)
R=.Ulf, v Z.-Institut
1959
ARS jourml
Vol xxx, NO
Nov ig6o
11

62-14005
Golitsynakaya, E. D.
CERTAIN PROBLEMS OF STABILITY OF THIN 1. Golitaynakeya. E. D.
CYLINDRICAL SHELLS (Nekotorye Voprosy
U6toIch(vo6tj Tonidkh Tsilindricheskikh Obolochek).
119611 [231p. (foreign text included) 5 refs.
Available an loan from SLA 62-14005
[110LIgh (h-Aftl tfiIII.I. of [Akademiya Nauk-SSSR.
Institut Mekhajilki I.. Inzbenernyi Sbornik, 1959, v. 25,
'Ii. 145-153.
DESCRIPTORS: 'Structural shells, 'Cylindrical
bodies, Stability, Load distribution. Deflection,
Theory, Numerical methods and procedures, Partial
differential equations.
The Investigation Is based on the equatJoY of 'he
linear theory of thin small-curvature she 's. COL.
elderation is given to the stability equation, =P
(Mechanics, TT, v. 7, no. 7) (over) Off1cw OT.4:hnical 5-fca.

Investigation of Heat Exchange in
Supereanic Flow of Air In Taboo, by
A. S. mamnavt 5 pp.
MWIARy per$ IuzbmpMZ&_Ak2Mp
j
Smj,
XV) 1959..
ARU Jmrma
Vol la go 11
NOV 1*
/ ?.I,

Movchan, A. A.
BEHAVIOUR OF COMPLEX EIGENVALUES IN A
PROBLEM OF PANEL FLU17TER. [1962][II]p. Iref.
Free copies available from Boeing Scientific Research
Labs. LAbrary as Boeing Trans. R49. When supply is
exhausted, order from OTS or SLA $1. 60, 62 -18856
Nauk SSSR. Institut Mekbanivi
vi~
ik
n 960,
Sborni
r y
DESCRIFrORS: *Aerodynamic configurations, *Panels
(Structural), *Flutter. Supersonic characteristics.
Numerical analysis, *Complex numbers.
62-18856
1. Movchau, A, A.
U. Boidng-rranv-1149
Ill. Boeing Scientific Researcb
Labs., Seattle, Wash.
in the problem of the flutter of a thin. elastic, rectan-
gular panel, moving In a gas with great suWsooic ve-
locity, results of additional calculadons are given for
the region of high velocities, iff which the eigenvalues
of the corresponding non-self-conjugate boundary value
(Mechanics --Aerodynamics, Tr, v. 9. no. 4) (over) Ofte of Uckokal Seftu

On the Elastic-Plastic Stebility of v
Stvacture Tneorporatim Bars, by A. A.
11yushin,
RUS,51-AR. p2r, IX lazbeneryl Sborak
01
Itw% Otdol Tekh
pp
NM M-3320
Set - Phya
reb 62

Mikhailov, V. V.
ON AN ANALYTICAL REPRESENTATION OF THE
THERMODYNAMIC FUNCTIONS OF DISSOCIATING
AIR (0b Analiticheskom Predswvlenli Termodinami-
chesk*h Funktsil Diosotaliruyushchevo Vozdukha) tr.
by John W. Brook. May 62 [17 ]p 2refo Grumman Re-
search dept. rept. TR-21: AD-275 816.
Order from OTS, SLA, or ETC $1.60 TT-63-23478
,Trans. of [Akademiya Nauk SSSR, Institut Mekhanikil.
tinzhenernyt Sbornlk, 1960, v. 28 (Abstract
available)
DESCRI[YrORS: *Thermodynamics, 001asociation, *Air,
ChemlrAil reactions, Excitation, Temperature, Energy,
Functions, Gases, Partial differential equations.
Molecules, Enthalpy, Entropy, Specific heat, Gas
ionization, Gas flow,
rr-63-23478
I. Mikhallov, V. V
It. Glh'r-TR-21
111, Grumman Aircraft
Engineering Corp.,
Mbpage, N. Y.
IV. AD-275 816
(Physics--ThermodynamicH, TT, v. 11, no. 2) (over) 01 Teefivic3l senlro

Do
RWA
IT JU 60 w
Effeft of CA un MWAWAOW
P=VU-UIM Of 0=4 UDOM by
1960
randmi, pro IVOL28*00M.P/
umv0d MOT-133 -* (za)
iml. SU solobles, 04b not tmlte Id bi
pp- do not =rLUaWp

Effect of Fadioactive IrradietAcm an the
Mechanical Properties of Solic?A, br V. S.
Ims-kVI, 39 PP.
RUSSIAN., per, kAhen2MM, 'I Vol 28, 1960.
PP 97-12-3.
JPFS 46209
sci-Mat
Sep 68 365,439

On the Strength of Thick-Walled Cylindrical and
Hollow Spherical Shells Exposea to Irradiation., by
A. A. Illyushin, P. M. Ogibalov, 15 Pp.
RMSIA1, per, InzhenernU Sbornik, Vol XXVIII.,
196o, pp 134-177-9-7736d
FTD TT-62-719
Sci - Physics
jan 63

Propagation of Elastic-Plastic Flexural and Shear
I
liaves in Axisyrdmtric Strins of Shells of IWvolution,
by M. P. Galin, S9 pp.
RUSSIAN, per, Inzh Sbornik. Vol 31, 1961s pp 136-170,
AEC/SCL-Tr-252_-'ff_
sci/phy
Nov 69 396,002

lj~-~IX36 ceoloa Gna waxomoloo, by 1-1, YM
Bk
rMSTM, j;LG', ltruv=
1957, pp
OM60-23%1
PLJO
reb 61
PST No. 133

EngineeTing Psychology,,
i'luSSIANS bk, Inzhenemaya Psikholop&a,
1964j, pp 1-396 (c/c)
*170-dT-66-147
Scillingiiecring
1~) r G6

11algincering Seismology, 6 PPT
U, Inz1henernaya Susnologiza
1962.
ACS1 1-6837
IV 2204011765
C r- -'r - "7.5, -, 7 a 0 //
trisk
~ki/Lagr
*'j,u) 66
293,011

63-12190
Unksov, I- P.
ENGINEERING THEORY OF PLAsnaw 1962 IV. 1. Unksoy, I- P.
order from Butterworth Inc., 7235 Wiscon;in Av~., I.I. Butterworth Inc.,
Washington, 14, D. C. $13.00 Washington, a C.
Trans. ofmono. (Inzhea=ayaTeoriyaPlitstichnosti;
Metody Rascheta Usilif Deformirovanlys, Moscow,
1959. 327p. 1.
DESCRIPTORS: *Plasticity, Theory, Engineering.
(1viechanics, 'IT, v. 9, no. 1) Offlet of Tockmkol Servicis

63-16632
B010tin. V. V.
NONLRflM Ft.Vff ER OF PLATES AND SHELLS. 1. Baddhk V. V.
119631 371L 19 refs. U. BoftTrm- R45
Free oupies available from Boeing Scientiftc Research M. Boeft Sclaulft
Labs. Library an Boaft Trans. R45. When supply Research Labs.,
Is extausted. order from WS or SEA $3.60. 63,16632 seaule waox
q &AM=-bWU*44*khu"
. _k
Y. 28, p. 56-75,
DESCRUTORS: OPlutter, . *Masdc shells,
Stability, Supersonic flow, Gas flow, *Aeroebaticity,
Fluid dynamics properties, Ntonerical Maysis,
Aerodynamics, Panels (Structurao. Structural shells,
Aerodynamic heating.
7U su* is devoted to an inveatiptLon
flutter of plane and curvilinear paneb.
there to a flow with great stqwrsadc va~iEe~v awit 1.
OvIechanics-Aarodynamics, Tr, T. 10. no. 5) (oveli MCI 01 Tfthmkd in"

I ille le Act on of an DTIO.)._*10r,
(11' tL
Concentratod Marcos in U, form :1 (Homo3encous)
G110tind by V. V. wir-sor-ov, R. D. Stepenov, J-4 pi).
12.4,11 Ah
11.lauk 5SSR, pp U7-"". 9097
AEC SCL-T-392
Sci Bagr, P)Yjz
Apr (32

On the Strength of Thick-Walled Cylindrical
and Hollow Bpherloal SbaLls Exposed to
Irmuationo by A. A. 111yuhin., P. M.
O&Lbalm) 15 PP-
=SIM, per, Inzb9me=Iy 80=uM Vol
M=j 2,903 WISV:114- ;we6
pm-m4g-m
861 - ftv, Ift
JOA 63

Rolling Moment of Flat Wings in sm Oblique
Supersonic Gas Flow, by Yu., 1. ftwiltatkov,
17 pp.
RUSSIANI W, Inhwon?ry Sbornik# Inst
%kh A Nauk $99 "O.61,1WIM
pp 9669M
FTD-TT-63-402
Sci-Aoro
Aug 63

the
lu overma" I" ruws
it A- Ise

Sci - Phys
Nov 64
FOR OFFICIAL USE ONLY
269,068
M'..
I li

Sci - Phys
Nov 64
FOR OFFICIAL USE ONLY
26t9j070

Zhigulev, V. N., RomislICYSkii, E. A,
and Vertushkin, V. K.
ON THE ROLE Or RADIA71ON IN' MODERN PRQB-
LEMS IN GAS DYNAIMICS (0 Roli IzIuchenlya v
Sovremennykh Voprosakh Gazovol Dinamiki). [19621
45p. 20 refs.
Order froin OTS or SLA $4.60 62-20138
Trans. of -Inzhenernyi Zhurnal (USSR) 1961, v. 1,
DESCRIPTORS: *Aerodynamics, Fluid dyllaillICS,
*Gas flow, Temperature, Tbermal radiation, Black-
body ridintion, *Radiation effects, Hypersonic flow,
*Aerodynamic configurations, Aerodynamic heating,
Recombination reactions, Equations of motion, in-
Eegrat oquations, Differential equations. .
62-20138
1. Zhigulev, V. N.
11. Romishevskii, F. A.
111. Vertushkin, V. K:
(Mcchanics--Acrodynamics, '17, v. 9, no. 9) office of Taftcal Services

The Hypersonic Area Rule, by I%L D~
RUSSIAN. per, Inzhenierniy Zhur, Vol 1;, No
'j 9679781
PP
FrD-TT-62-1311
63

ConcerninE; the Calculation of the Nolecular Com-
position of Air For a DeteriuinatiQn of the
Coeffecient of Aerodynamic Forces and the
Ttmperwt.uxe of the Body in a Free 1,1olecular Stream
at High Supersonic Speeds., by V. S. Galk!~nV
RUSSIAII, per, Inzhene~M Zhur, Vol I, No 1, S9627
PP 175-176.
TD-TT-63-361
Sci - Engr
Mar 63

on the stability of Obationary ~btions of Bingl
(gyroscopic rvd.ces,, by A. P. DxmMni 13 Pp.
I= TAN ? per, Lnhenennyi ZhLw, Vol 1, No 21 1961j,
Pp 16-30 .
CWFW X-4859
Be:l - Ailys; Ew-
Apr 62 19~21 17,1

Flow Round a Plate Noving Thrmgh a Shockwava, by
A. 1. Golubinskiy.
RUSSfAN* per. Inzhenernyi Zhurnal, Vol 1, No 2j,
19610 pp 26-id7~
AEC AWRE-tr-51
"V, SI)
(/,;j ez,~(? u 7,1 et,-d
Sci/Engr
Jun 66
302,552

Buckling and Steady Flutter of float-Compressed
Panels in a Supersonic Flow, by V. V. solotin.
RUSSIM, per, Inzh Zhur Vol 1, No 2, 1961,
pp 82-96
NASA Tr F-10g,106
Sci-phys
Jul 66 302.150

Forced OscUlatiam of Plste* v:Lth a LoeA
Represmtift a Spoe-Tift PrMe". by
me Fe Dimtoms 18 ppe
AMIM, per, -- - I I I I a I mmmalo Val 11
No 2p 1961., j~ 9T-105.
PloolNO68-V
pm-g-r-66-CAS
SOL. bpi"
Julfbo 36o.670

Natural oscinatime or primatic she, is of
the Monoooque-Type AirpLme WIM In a OLq)er-
sonle Air Flows by A. 1. Yelpatlyeveldys,
13 pp.
RMIUs per# ZWMIO VOI 10
ND 20, 1961.0 pp lWill.
Piool3To68-v
FTD.HT-66-"8
Sai-Aeronautics
July 68 36D9671

on the DjaWo Mbility of Shallov Blutle aheUs. by
G, V. wichea0vo 8 pp.
RUSSIAN, per., Lizhmumn*7 2b=., Vol 1p go 2.$ 1961)
pp 112-118. -
CIA/FM XX-.U43
NOT MMASABLE TO FORRM NAT=ALS
sci / F-5-~ 9 A 0
may 62
usn nnmm un MY

rr-64-IM
Keldysh. V. V.
rXACT SOLLMONS FOR WINGS IIANqNG ONE AND
TWO PLANE SHOCK WAVES (Tocbnye Resheniya dlya
Nesushcldkh Sisterr. a 0dalm i D-,umyr. Plooklml
Skachkaml UplotaeWya) J. W. Pabwr, cr. Sep 63
125p) 5rds RAL lAbrary Trane, no. 1044.
Order from OTS, S'-A. or ETC $2.60 77-64-13333
Trans. of lnzbeDemyl ZhLwul WR) 1961, Y. 1, no.
p. 22-39.
Abstract trans, is ava.Uable from OTS or SLA $1, 10 as
n'-62_32111, AM-62-94, 29 Jun 62. 2p.
1. KakWih, V. V.
H. RAE-TrazLn-1044
UI. Royrl Aircraft E=ablish-
ment, Farubmugh
(F,ngland)
(Mechanks-Acrodynamics, 7r, Y. 11, no. I(Y) Ottke 0 T.ch.1r.1 S-ic..

cmemiug an AboDst FM4blWdlw Mir Of
Rwafled Ow ftat it DOUOSP bY R- 13-
irosmlkm,t 9 PP.
FmsTm~,pyw.j, igrm%~Wv Vol Is
0
w
, 1,
So 3p 1# VP a
IT041-43-50
WI.Mw. OV.?
"ef.6
govi 63

Calculation of a Turbulent Subserpd Stream of
Real Gas, by V. 1. Rskulev. 17 pp.
RUSSIM., per, 1"ienew PMAIS Vol It No 3.
1961, pp 6S-~477~0441
FTD-TT-6S-1923
Sci/Guel
Jun 66
302g536

Mil not -~M= at * YA*r In a nobwp
T. so Oomp 9 pp.
15MIA% WS Vbl rio 1b 3.0 19( AL.0
.1 - -par#
IV 3&-*. -
ad4hp
I ft 63 gy 3 S'7.sl
lp

.- ----16.A of
0004"bg an TARDS Of mammu ~w
mal.t
asioxatum MASI of semen
DIE gm t 4 1, so Odkins, 8 VP-
W-- 1w
~~ 9w ONO* vtgL 16 lb 30
0 It 33 ~V~
sol~ A31~r7y
88963

am rim with onummm JU egm vith POMM W&WO
by V- l- UWWns 9 We Vol %A, No 3. 1961-t
aw=# )r-Tt
pp 20-Ima
so:L . cbm 2/(0" eh;
mV 62

Oa the QuestIon of the E8timation of the Walking
of a Balanced Gyroscope in a Czwdan Suspensiouj
by V. V. Kvementulop L. M. Markhashov,, 4 pp.
PNUSSIAN2 per,, lnzb ML?b
1961, PP 3-3. ~Urvo:L 1. No
cWkw. xx-1146
NOT MMABU TO A*6910 i 1W
Sai
my 6
US-P.- MT-MITAT, IVISITY, MY

Aerodyawdc Characteristics of Wings in a Super-
sonic Flow in RKU Presence of Slipping, by
Yu. 1. Krasillnikov, 10 pp.
RUSSIMO per, Inzh8nOm7-qTF,,.,Vdl I* No 4j 19610
pp 18-260 96W01- - - -
'76 F 67 9 -2-
ffD-TT-63-388
. Sci-ABTO
Aug 63 JV-2"' 0 ~ r

Vaporization of Solids by Absorbed Radiation
Enargy, by E, M., Shakhov, 23 pp.
RLISSIAN,, per,, luzhcne~myy. Z
#rnal, Vol 1,
So 4, 1962 s pp -2741f.- 69S047
~ eS6 75, Z
FrD-TT-63-77
sci-Phys
Aug 63

Turbulent Mixing of Coaxial Flows in Constant
Gross-SeQtion Channels, by 0. V. Yakovlevskiy.
RUSSIAN, per, Inzhenernyy Zhurnal,
Vol I, No 4, 1961, pp 39-50.
*FTD-TT-63-1139
Sci - Engr
Dec 63

I t stream Ifith
"I fTs"iffiras OYTV" C&~"v P 10 PP.
Rfgfl 0 0 0 0
RMIAH. per InZ-49A#IW,, Z4"0 Vol 11, No 4.
'f-'16
SI.S . W091
1961t RP -
WV2
FTD,7T-63-388
sci-Phys v ~ -~,Oy 39
Aug 63

on Waves-Starting Of SuPersonic Diffusery by A. I.
Lashkov, A. A. NikOlskY-
RuSSIANI per., Inzhenerno Bjw Zhur) Vol II, No 1,
1962, pp 11-16.
*FTD mT-63-32
Mach.ine translation
13 Aug 62 -,q ~v 'S q'i (111qp L ~ 0 /
/~ 11

Heat Exchange in Turbulent Boundary Layer of
Compressible Gas at Longitudinal Pressure Gradient,
by Yu. A. Koshmarov.
RTJSSIaN, per, Inzhenerno itU 2hur, Vol II, No 1,
1962, pp 41-54.
M
*FTD AT- 3-33
Machine translation
13 Aug 62

Turbulent Boundary Layer With Pressure Gradients
on a Porous Surfaa. by A.-I. Tolstykh, 14 pp.
RUSSIAN, per, Inzhqqqn)Y_Zhur, Vol 11, No 1,
1962, pp 79-86-.9668531
FIV-TT-62-1694
Sci-11hys
May 63 ,vie;:gj9

Ite Processes of Iodution and Recombination
in Hot Air, by V. A. bronshtns# 14 pp.
RUSSIA Ni peri, In Vol 110 No 19
1962& pp 16 0. 966BS31
Mift-62-1694
sci-phys-
may 6i

Aerodynamic Characteristics of Delta Wing
I
.1ith Deflected Aileron, Flap, and Other
Secondary Control Surftces in Supersonic Plow,,
by Yu. 1. Krasil'alkov, 13 pp~
RUSSIAN, por r. Vbl 110 No 10
19620 pp 175 181. 9668551
FM-rf-62-1694
Sci-Aero
May 63 ';~ j

Research of the Stability of Bimetallic Cylindrical
Casing During Axial Compression Beyond the Elastic
Limit, by V. I. Korolev, I. G. Smirnov.
RUSSIMI, per, Inzhenernyy Zhur AN, SSSR, Vol II,
no 1, 1962, pp 98-110.
*FTD-mT-62-53
Sci - Engineering
oct 62

Application of the Asymptotic Method of
Certain Problems of the Dynardcs of Vehicles$,
by V. A. Yaroshevskiy, 19 pp.
RUSSIAN, per, x Vol 11,
No 2, 1962, pp 2 1-221. 9668491
"D-rr-63-164
Sci- Math .~ 0 19-/ (4
May 63 A

Strong Interaction an a Plate With Consideration
of Slip and Hear-Wall Tmprature Jumpg by
A. A. Sopdove, V, S. Galkilkl 13 pp,
RUSSIM "-4Amerqyy Zhur, Vol II, No 2. 1962,
pp 231-235. 969uff-~
MTr-63-304
---Wpm
Sci-Engr 7 6~-17 K3
Jun 63 OTS 5-
$ ~ jpL

gxperimental hrrestigation of Heat RmW2aqp
of Flat Plate in Supersonic Parefied Cam Tim,,
by S. I. Koster1m) Yu. A. Koshmaraw, 13 pp.
MOSTA., per,, lobeam, 22mul Vol 2., No
2y 1962p pp 263469 PlW303267
PM-MT-67-43
Sai-Pbysics
Dec 67
344j430

Convective Heat Exchange in Supersonic Conical Nozzles,
by Ye. U. Repik, V. Ye. Chekalin.
RLBSIAN., per, Inzhenerno Wmo-Zhur, Vol II, No 2,
1962, pp 359-364.
1
*Fm TT 62-36,
Machine translation
13 Aug-62 I-W
~-6 qIg pL ~'q 0

[mistance Crisis of the Diffuser, by
A. 1. LasIdkov, 7 pp,~.
RUSSiM, per 0 InzIlenem Zhur Vol 2.
=60
No 20 19623, pp -36S-Mg 907085
FTD-IT-U-1202
Sci-Engr
Jun 65
2820224

Hypersonic Flow Around Thin, Imliptical, Blunt
Cones, by A. A. Govacheva, M. D. Ladyzhenskiy
RUSSLVII, per, Inzhenernyy 7-hurnal, Vol II, No
i962, pp 14-26.*
S
Sci - Phys
Feb 63

viscous Hypersmic now Past a Slender Cone,,
by V. S. Nikolayev,
RUSSIAN* PP-rm, Iumh- Zh- Vol 11. No 3. 1962.
pp 9-13, P?/Oj&
NASA TT F-485
Sci-Phys
Jul 67 332vg7l

Hyperaouic Viscous Flov Around a Slender Cons, by
v. s. NjkaWv., 6 pp.
RUSSIAN.. per, lmzb ix Mur? Vol nJ* No 3, 1962,
pp 9 -13.
CM/FM xx-1308
NM PJMMASM TO FMON MnONM
varg nm uss omLy
Sai - p*8
ix-c 62
217,260,.- -

Plasr...a Acceleration by a Magnetic Field, by
S. I. Fadeyev.
RUSSIAN, per, InzjI)en.ernYy Zhur, Vol II, No 3, 1962,
v
pn 68-73.
Sci-Engr
Jan 63

Scl - Engr
May 64
2670669

scl - Engr . I .. . I
May 64 ... I .. I q
I . 1 207,670

Sci - Engr
May 64 1 11
1 267,671

Scl - Engr
May 64
267,,669

Electrical Dischargo in waterp ~y
N, V, Fillipava V, Yo Zhurin, at al, I pp.
, ,,Zburp Vol Ila No 4a
RUSSIM, pora Ino .
, MxW
1962, pp 341-At" 060*
FID-IT-63-SU
Sci-Engr
July 63
Af 4 P /, f

ftte !f Cbrdcal Rezjctfon wid Its Itrfect an the
Prvyx-?is of Droplet CcmhuaiOn by V. R. KuznetaoV.
6 pp.
2naTAI, Vol 2, No 4,
rwx~ Z.
196-e# pp A-349- 96&1224
M-IT-6,1-653
Sci-Chem
oct 63

An Experimental Study of the Enthalpy of Tuhg3ten
Within the Temperature Range of 350-2000*C.-by
V. Ya. Chekhovskol, B. Ya. Shumyatskii, K. A.
YOMMOViCh.
RUSSIAN,, per,, Inihnz Zh Vol S. No 10, 1962*
PP 13-18.
AEC ANL-tr.451
sci - mat
Sept 67 342,1279

VOL -3) 1 q~43
IMME11161 = io'bl thly
Ugn
(Soviet Engi I
Translation of 1963, Vol. 3 to
1965, Vol. 5, No. 2
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