A FR: SKHARANAYA PROMYSHLENNOST TO: AF USSR. INSTITUT AVTOMATIKI I

• Document Type: CREST
• Collection: Consolidated Translations
• Document Number (FOIA) /ESDN (CREST): CIA-RDP91-00772R000100120007-7
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 91
• Document Creation Date: December 29, 2016
• Sequence Number: 7
• Publication Date: December 31, 1983
• Content Type: ABSTRACTS

t1so of Associations in Food Liduitry Izlulod, 1,-,r
G. Dlusai'lrov, 5 PP.
RUSOIAlil per, Oalcharna-ya Prcrwshlennost'. II~A;Oscovy'
1,-o 4, 1972, pp 48-50.
JfTs 56007
iAY 72

,:T1 i;!!!t
Akbavl Nlannotilt
6 19P2 Z-f3~-;U

Vt

Su7l~..w Boc-t Pricing Procedure Chalri~-,c Proposed,
1) -,,r 13 . N . T o s t e I, , 9 p 1) .
RUSSIAN, p(~r, qa'Kharnaya Prc)mv--,!,I(--.nnost' ,
!!oscow, 1:,:) '1 , Jan 1.1.173 , -)1- '-7
JPPS 58373
I'lar 7 3

Pr6blovis of Sugar Beet Supp-'~y Discus:;od, 10 py).
, SIMI, por, ~;,-Ilcharnayp Pronyshlexil-lont', i-loscow,
'U.S, -
1
NTO 4**', Feb 1973, PP
Jl'iL5 58503
APr 73

Measures Advocated to Improve Bitgar F"t Harvest-
lq3 In soviot uniono 10 PP9
M;SXA'N, per,, Snkhemn s1rana, No* 1P., Dee
1966., pp. 29-32,!
JPRB 39722
USSR
sel-Ag-l-le
Mar 67
.117.,287

Summ Beet Production LummOxe, in RsFsRo
by Vo Go Xatsonko, 9 pp.
RU&PTAN* per,; jW ~x
.dmr W S
, mk2p,.9 Mog;ccnjo
NO AAI 19691, pp 134t.
alras 496z4
jai-Agri
'an '?a 3990425

a*ar Jamot LAU19try orderod to 1--,~Ociernizsjo
r, pp.
RUSSIAlis port 2LI"..-rnm . k1al, Mosomyo
No lit 1969P pp 38-39.
JMS 49651
Soi-Agri
Jan 70 3990472

1. V. Radchenko
An-2 Airoraft. 645 pp.
RUSSXAN, Swwlet AN-' 1969, pp 1-440
AIRIFTD- 24-36-71
eept 72

CanstrucUon and Operatics of Th, fill-24 Airplme,,
by 2h. S. Quo=vrihop at. 61. 564 pp
ma .1 bookq .*.
�A MI-A
Akmawtat 19 P2 1 0.
--.44
AIIWTD-HC-23- U-69
sci/aeronautics
feb 71

an Lnotimmont fov MeasLaIng the Instantawme
Torwemtw"as of Gas lamal, 17 D. F. Slmbirakiy-7 pp
per, Simolotoirtri " -. JL Tol.
20 19659 ipvp 5
VTD-HT-23-874-67
sci/phys
iWis 68 3598-318

149hsa CiNUPUtOT of Odmotrin Charactoriatict)
Sootima 1401stiva to Contirza mms, IV
lomi3%tss 8 pp,
RUSSIAN,, paro �mRgptogtxvY-a i Toldmika
-yombftolTo f1plao NO 91-W.
P100221368-V
F-rD-fft--23-S9D-67
lsai/Bloot & Elect Engr
$opt 68 366v62.0

Invostigntion of tho Elffoct of tho
Dofomtitlon Rvto on Corrosion
ot Hot,!,Ils, by V. G. 111(onc-nor2lco,
IMSSIA410 per, Samletstrmrliyo i
Teklmilm VozdushnoGo Pl tri, iTo 1~, 196.r',
pp
Al U/1'"MOY-C-23-1152-67
AD 67723,5
sci/materials 353,213
J,q n 6 19

Calculmtion of the StabUilty of Circular Solid
and Annular Plotes by the Discrete Method vuth
Uniform and Nonuniform BDundary Conditional by
Yu. P. Petrov. 17 pp.
RUSSIAN, per, Samoletantroyaniye i Tekhnika
VozdushnoKq -',,71ote, No 4, 1966, pp 39-51.
AIR/FMAIC -2.3-435- 69
SCL-Phys
Jul 70

Aximl Compression of Sandwich CylinftTv and Pancla
with Corrugated intorplayer and l3lactic Fromen,
by It. A. Pannachko. 14 pp.
,e L Toakhniki Voz-
RuSSXM,, per, SmDletestrwi tiV
dushn2go Floto, No 4. 1966, jkp 52-61.
AIR/M/19T-24-316-69
sc.-;-
JUne 70

The DevelcprL-nt of the U-Lecretical Principles of
tho 'vbluiv-tric Dafo--nuaticn of A'.btah;, by
Yu. N. Aldcrcycv. 7 pp.
;Ip
WS.LVI, Lx-,r, Sanulctos
Vbzduslinogo Flota, No 5, 1966, pp 32-36.
. 1 1.1.0 1r-23-128b-68
UT
sci/ materials
nuv 69 397,059

Tho Operation of an Air-Fecd Jet Ca:11bustion
Chamber Under Unstablo Conditions, by
1, 1), C~oldaycv, A. 11. 1,,otonenkc), d pp.
RUSSIAN, per, Sanolotostruz,ciii-ya i Teklini-ka
VOZIJUS11311O.P.0 I'lotill No -So 19609 1y 59-640
AT 141
Sci/Pron & Fuel
Nar 70 402,59b

12-9-3 TIT61-10-234
Expari'loelli-Al invebti~,ation of the condiLions producin-
rotat.ing 3tall zane5
Ptuis pur. mr,oletostroyeripa i t.ekhr4ik,-. vosdu,5hno-O flota,
110 5, 1966., ?3-76
4( 7-0 - 1,!17- -/-L/, S'

A "itiuly of ."'haping FroccDoes in the Produvilon of
Avlwtion Candult Vlangaso by A* A* lelotat 5 ppe
MUM, per, sampletostro2ecrAya i -.4slchnika
vozduslmoEo -F-I-Otmo No 59 1966, PP 13T.1420
A:ER/I.TD/ii-i-23-1305-67 AD 679 662
se-i-i'lacli
Feb 69 3MM

Electron-Ileam llmting in the Far-dng of 6hect
,,V:sterials, k, 0. G, Korolt, ppa,
RINSIM, par, Samoletoct axenil, 1. Tekkrr4
.,r
m
VO ushnoigo F-lota , NO 5, 1W6 9 PP. I
AIR/r,TD/ItT-23-1365-67 AD o79 c D
Rliech
r,-ob 69 372- 9922

110100 !(OdUCtiOTI ill ;Vroarj of Tll--.121~
Airern.ft Takeoff,, by 13,. 1 1. Mel I nill-ov
ffussl.All., b3c,, Samolctost,',-_oYolllY I
Flota. KI-lartlaw
Tolrluilka
3ASA TI' F-11,557
Scitlioro 369.,o86
Oct 108

Experimantal Installatim and Mothod for Ccn:-
ducting Ex4vrimalits to Datenlino Fatif"W Limits
pf 1111101inu Cumoctions in Urcraft ilydraulic
Systevs, by L. 11. LozitsIdy, A. A. Ivanenk-o,
et al. 10 pp.
RUSSIAN, per,, Sanoletostroyomyc i TeMmika
Vomdusbnoi~,,o Flota, :J0 pp 82-89.
All 17 1 --,r U 7: rf--21- =37-- G 7
scilimchan enga,
mar 69 376,,644

Motb~,d of Dstarmimtlan of SlInalpa of any4c in the
Proooss of Stanqxtngs, by A, 1, l,ojxtjn,,
V, 0, Katulyan, 6 pp",
RLMUN9 pDril Samlatostrovni- i Tekbaika
yamj~qvhn 0 ota, lJo 69 -19669 pp 10?-109.
P100185868-V
k-TK)-,mT-21j-12q-6?
sai#%t
Sept 68 364,898

wtarzLi4tions or voioeity ataa ami liatum of
DaTarmati=3 wbon Frewing Ilircgli a Roelantmlar
Dies by To 10 Glebovs 7 pp.
RUSSIANg pers I Talclu4ka
No 69 1966s pp 120-123.
-V-Q 4-01M gta,#
04 Pao a -
PIOOI8586B-V
FTD-INU-214-129-67
scd/l,.;at
S 68
9.

w-wril-Lblatiul Oi the - kai~, -*It*, Of ;.:q1 !~,iljl:
y i"'ircr,li't
i>y ~-'jethcxi-; of :;LiitL;Lic~i, oy
;,~. A4 13 1.4, ~.
per, l-;a.r)lqtos4(;yU *-Y-,:! i 113~jlllika
vozdxt;imo~jo Flota, "0 7, B66-, :)~p 3-M
;LT;Vl- D/~!i"24-223-ljlb
sci/nab-la-l-.1 sci.
fu, ) 69 .3 -b , 6 4 8

Certain i~,esults of tiie ital
aintim ut' Arfoil ai pyusmar cmack!-, ~,'i-tli
Yu, V. Aepwluv, 6 Lip,
Par,
1.10z"Watul0c . ~~o 7v 1-90G, 2VY-31
U17
r'~- F - J/ 'L13
sci
L--b 69 375,,6z.D'-

i:ut,--riT-jj)aticsi of: bue BorLkar of Stablk-- C~xrarat
of Sta~s of an ;Qdal Ccxj.)n,-!;L;or ))y tin- Cal-
cul"IticAl ;-b-WlcxlF i~y Va
Vo J. ut ai. 8 j);.).
Vmdusiulot'o i~lota .c) 7, 1-966, pp 32-36.
-21,24-68

of tju.~- Pmlimcl of i~-,pliaatial ';tuzs,--s?
CHI of Ule :AaUmq-ul 01.,
"alpy Ji;95, by A. V. l~aXIa-sildlov,
V" ~-. 'I'ckarev. 9
C-11
lvlotas A&--7-- 66, 9-.
1 cr"I ~77113/' '11-2 4-2 2 4-6 6
s ci/-,: k1be xi ad
bab 6 9 375,651

alba of Pricticti in C(i.,,~crdtr-
Loarli-v '):,.o hy [;. 1. II-r0chill 6 pp.
R.) 8,, L466 p,:.) 3-6.
I.VFlA)1II lal-23-50,13-6 8
sai/3-ocitan oJ-1c.)r
71-ar 70 402,19 806

FTb (TDP-, 11R ,T,)t--6A-ic-?61'lT
Sylithosi'l of ituirti-murn-vie ight cTl --i 3. ca - -3 taS
'R abchen)m V. M.
LY
Rus Fl~r: Sarroletostroyeniye toklinil-a -.rozduslir-og*,)
flota,, no. S. 1966, 8i-80'
,Q, 0 IT

OuTent-collipator Contact thwUrej, by
V. 1. Kormil-Ov. a VD.
MWWp b~&.p Smalst i Tekbmf ke
Vbz&upbnq,gR Matup IWj, pp 105.
NASA TT F-3.2.,5M
Sol-Elea
Jan TO 399.1013

CptL-,-u,,, Cylixtclilcal ';Mddcil
Coru -'LUf-ujv-,d by
Fra.uo, I)y Be ivo
) K.~Kp
V(zdu-ll u lo, a,) I'lC)tap Liu a, LIM"77 lol-D5.
It
M".17-TUTT 2
U Cl k a I (aL x;r
-;oi;L 0
393,009

,:dj,t~ jjjCjU3j,)~,j I.LU_
Ative Lattice 01, an
Jt~ttaaxed kmsor Durim, t-J-u-- Ualfoniatim of cmi
!:A'-Icnknit
10
I.,10ta i4o 6,, 195c), 77 11,71- 5.
may 69 331,265

!'A-ierirrental sbucil of an oscillator( I.,voces!, in
Cylindrm-d Excited by histaktalemn
I!Wratim of Mwr p Ye. A. lir-bery,
F* licadiev, et al. 13 p~'.-)O
Vbzduslu-l(xp r Iota 8,, 1966 ri 14L
69 381o,167

-~olisi-Lijic~ ij,~my? iiaws for j-dycraft
~x~x~iy cinci L'
oy Vo .1, lbru-mb" it. I'llictkolov. 9 I)IJ.
-;,v-xActa-itnV(!TLiYQ i '110MIniki-I
Vb2ch-nmuickjo r'lota, ~',!o 8, 1966, pi-) 16C-173.
~ ~
'Vilp: 1~-24-4~368
cm,.jr
july 69 384,220

ThatoodynamLew Calculation of acactlon-l)~pa Com-
bustion C%mokboirav eunctioning on a e-umi of the
Type CellhOoNn with a Coefficient of Z'ucess Oxidizer
,:% -- It by 1. P. GoIdayev# V. P. Merepanav. 8 pp.
Lva -1 Tekh
6USSTANt part SozolatopIKUan - nika V0Z-
duchno&2 L-lota, No It 19679 pl? 11-16.
jUR/FMAU-23-603-69
Sci-Phys
Jul 70

Selection of an Optimum Means of Realiz-
ing. Control Algcrithmq for Aircraft Com-
pisters, by N. 1'. Berezyuk.
RUSSIAN, per, Samoletos-Lr2yeniXe i uki,
Vozdus1mo8o.F1otn, No 2, 1967, lip 45-48.
NASA TT F-12,000
SCI-Elec
Mur 69 377)PS44

D~,Nattm--4:; ok 'Lie i>rocs--ss of q:)tiiizaucn of ijjc~j
l'1.1;(:hrl=,Ik~; Pli'Jit" by yel., P, vadl~,.uov, 9 j )" 1.
ikll:, yo i
1,'fota, jc) 9,, 39617, pp
M 17771, 71"T-;M7-~6 ss
,,3ci/
(X:t ('39 395,264

"igirjeearby,l !I,-t:iicd of !~carW(nzmiic rxa~Agn of a
,.;rr R-ct M141iclk- ~ a Vx- - --'Icx,:
with jig)k T
tas tr
Vbzda,shl.lcx,O FJ=. A0 9" 19(;7,
77777:17,
sci/an- M.- -Iautias
july 69 3811;212-

.~:,]Lfbct of ~4,cxlulizondty of I-la., cla tile
Of tKI
FloLa, -.~o 9 , lq~; Av
269

Grinding of Inrge Platos and S 'hoots with a Variable
Cross Section, by V. N. Worevib, Yu. V. GcrasimcnoL.
13 Pp.
RUSSIAN, per, Samoleto-Stioxeniye i TeMinika
VozilusImm Flota, No 9v 1967, pp 125-132.
AMM/FMIC/Iff-23-163-69
Sci/her
Sept 69 387o426

3ilort 'I';*k-r-~Offs for Jet Ail-araft, 1v
,4,, ',,, 13 ij).
JA-ir, :*;~V!nj.~jxx3t:ayL-!jli~f(-- i
I-'Icjtao, .Io 10, 1967, 3-13.
~U;-V7.avlf.o-2 :,IIT--68
~Zci/ Lx.--ruilautia;
nov 6 9 396r996

L~m~~xinq ZEUiod for gvexnodynmic Calcult-e-
ticrus of jet-Type CbribWtial. chculbons Usiny
JJydiTy=bcn FUel cmd hir,, by 1. 11. (x-,ldqV-v,,
Ve 1-1, cll(-.Xm.)alov, 9 pp.
RLF.-SXPil#, perv Out ni)2 1 'IV--i-mika
Vczdu-glmq-q Plota No 10,, 1957, Lyp 14-179.
AElVlTD/!W-25eWH--6-8
sci/prq)
-T-Ir 69 3G'-OvO56

t-l-le Possibility oi~ ,~-ir C:oolillq
culbwticn ,bl~dllf i at
-1,, by 4101-damb 8 ;. ,p.
riat 1 -10
WeduLl In
J~-,b 70 402.,,134

7
(L- 9 397s373

Unstructim of Circuits of jwtcrk-tdc --,Wnal
Ac~ttor; Of PI(x%r caloitiens 'lac'ed cri I)
of Ilre-ssumb Distrilwticm Almcj the
by A. 'I, f-ki-dtary,mv
v. Yzi. et -Al. 8 p;-).
ilX~IIIAJP paro, Smolctostrcp Per i . ILA--X ILLa
I _, aye I i x
-Vc)zdmmno,-,o Flota,, ilo 10, 19617, -pr) 47-5=
`71:7-17
'-Ci/ electirida;
~L,c 69 398,734

ii i)iscrete ~"bUx)a of P3xite a-tict CalculaUct"t
by Yu, P. VotIM, 22 ill)
-"Impli3talt Nu - i Td-~iuw-~a
itaLtr-Im
vbzduslm~jo Plotat Isci 10, 1967, A) 5:P;9.'
1717 IT-2 3-672-6 8
sci/Llayi-SQ3
CA.) r 6 9 377,979

Bodl-le (Aurla) Glue Joiiit,, by r. pytioarets.
9
YO
Vlota,
-TWIL"23-1063-68
sc-,i/!:u-terLjjls,
july 69 384diS

w.,
COLIAJ,.~ 1,:j%;', ;Ay V, V.
IU 1 ").
Vcuc~w,'mic),,o 1'3.cta, -'u 10, 11167' . 7--U3.
M7/177. 777-1-~--5(TT-G~
s ci /z e m, - i - iu-Li c-
ect 6 !) a)311 -141

Hot Impulsive DefCTM81tion of Lvw
COTbon Steel, by P. P,. Kochetov%'
S. A. Poltarushnikov, 8 pp.
RUSSiAN, rpt, Samoleto~!~~Y_e I
To'm'-hnika Vozdushmogo FIota, No 10,
1967, pp 1110-IIS
AIR/FTD-H-i-23-316-69
sci Pin*_-A -, - A^' ^.-

The Optiv.um Incident Angle un Low-Aspect-Ratio
1,1(ptov I~Ja4lc!; of' a Cmiprussor ,Aago, 1)),
V. V4 Kovalovskiyo e) 111)0
RUSSIAN, per, Samolotostroyenlye i Toklinika
vozduslul(~,O 1:10ta, No 11, 196.7, pp 24-N.
i\ll."/!.-,L,I)/I,-rr-24-242-69
Sci/Prop F, Fuel
, lar 70 603
402P

11. of an Ercsicn Plasila sc~cc, by
Vo Vo Balyl.)c-ndn, J. A, i~d.~uiyak. lo pp.
111.3-SIMO jx~r# i 'Ibklulika
~ YLI
Vlota No U.. L(:Ib-/, v 35-4
r';.
IUI-Vl-TD4,-:T-24-173-69
jai 70 399s877

Evaluating the Instruction Pomat of a Control
Computers by V. A. Popov.
RUSSIAN# Imrs SamolatostronnLXM i Takhnika
V02ftshnoso Flota No 11p 19670 I)p 49-51,
AIR/M/RT-23-134-70
ScL-n
June 70

StAt-latical lawantlgaticm of' tho CrAwatimal
tooding or the landing Gem, ar u 1,blnvllrie
j,dr*ftft& by A. 14. PonflaN.
PXWIAIJ.g pDr, Saimplatostrmmn a i Teu-ulum
70 110 11
I-MA W :-,!m
sci
Doe 60 3719126

Rending Design for Elastic Ilates Of VO1riable
Thicknes5 w-ith Two Freo Opposite sides, by
YU, It, Petrov, 15 Pp.
Russ M. Imr, Samoletostroyew. 0 1 Toklmika
rjo I
VozdW! go FIRE. No 11, iqfi~' pp 61-7
ArR7fTM717~-42ff-69
Sci-phys
Mar 70
403,502

uypersonic Gas Flow Paot a Flat Plate %-Yitb
a Sha;q:) Loading Edge, by G. M. Poyerlintsev.
RUSSIMI, per, Samoletostroyeniye i Tekh
Vazdushnogo Flota,, No 12, 1967, pp 9-15.
Bept Wavy APL/JIIU CLB-3 T-595
Sci
S -rhys
July 69 385,267

Innuence of Smondary FbrcejB on the Takeoff
and Landing Characterlstl!a of a Short Takeoff
and Landing (SM) Jet A:trcnLftj, by V, 1. Surus.
MWXU,7 bk,, E~mletos . 4 yo i Tekbnika
Vbzg!!~oM Flots, 196T., yp 3.6-20. -.t < .-I-
NASA TT F-12#161
Bel-Aero
Sept 69 391.,528

Several Q=stions In the Seloatiora of Structure
of Flight Control computers, by V. 1. Popov,
N, T. beroxyuk. 7 pp.
RUSSIMp per5, SawletostEal ye I Tekhmika
Vozdwhmgo Flota 140 12 1967, pp 52-55.
V
AWM-4U-24-208-70
sci-Aaro
DOC 70

REQ. TR CHECK 28-w02-73 T278
EFFECT OF PESTGN SHAPE AND STRESS CONCENTRA-
TOPS ON THE STRENGTH OF UNEVENLY FMATED
TURBINE DISCS
KABELEVSKiXI-3 M G; OSTAPCRUK, I I; PROh-KIN,,,. A F
UR: SAMOIXTOSTROYENIYE I TEKHNIKA
VbZDUSkNOG,O ELOTA., NO. 12, 1967, 78-86 gqgps.
-ii J,

The Voa-tox at an Xnlot of an Air Intake,
by A. Ya. f4iroshnichenko,
RUSSIAN, por, Samolotost-royeniXe i Tekh
Vozdushnooo Flots, No 12, 1967, pp 128-20
clw R-W-995
May 69 382,285

fi.xperiment 01, the C"iditions of Cojlcci)tio,, of
of 'A!Ot-itint., "tall, I)y 14. V. Ile .lim, 7 pp.
UL1,S51004. por,, .;amolotostro-eniye i lickil V0ZLIusliftogo
Flotax "'j0 5, 1
Sci/Aero
1
Nov 6.
5959957

Approximate Mathoib of Calculating ths Distribution
of Velocity w ith Altitudo E-miring tha Braking of
Bodien in tho Atmosphere, bir 0. A. Privarnikov.
9 pp.
RUSSIAN, pars, SamoletostpMmIM i 7%akhniks
U-9ibelulogo Flota, No 13, 15)68, pp 10-1S.
AIR)M/aT-23-602-69
Sci-Aero
June 70

A Xethod of Covipensatiiig for the Amplitude
Fluctuations of a Signal Reflected i7rom an Aircraft,
by 1. V. Barystiev, 7 pp,
RUS.SlAN, porm Samoletost(voyclau i Teh-l-wika
Voukusimov Ffuta. N 13, 1963, D13 39-43.
AIR/ FTD/l IT-23- 210-69
sci/Elcc
4020609

C',u v'rn&s o.-l' Cu i-P utar Lovici2s for I-Iircraft,,
I-'IcyUi *,r) 13,, 1) 91-47.
GS
70 404,,45,3

A plication of Legandm- Tramsforms to cri
InvestigmtIon of Plane BlastoplOstic WE-.Nnatl
of a Loadj, by Turchenko,, V. Yno n pp.
MUSIAllp per, 8ampletrgen&O I Teldmika
Vogaughn 0 Flotu NO 13,, 196,61 Iv, 70-7b*
Al -21 ~-2 0-069
SCO%theiucttical Sciences
apr 70 ~g;, gan

Hxperimental Determination of' the Creep Character-
istics of Fiber Gloom-reinforced Plastics, by
S. A* Udovaz*4tv. 7 pp.
RUSSIAN, pars Sauoletrqztr~aeniye i Tekh Vozddshl-
twzo Flota, 1968* pp 97-100.
NM TT F-12,742
sci-Materials
Vlay 70

4CS(I-1-722520) SLONGITIA)INAL INIVAC
END FACE OF PRISMATIC RODS, CY)ANDRICAL, AND CONICAL
SHELLS. sEgorshin, A. A. IoTranslated by Patricia Newman
(Sandia Labs., Albuquerque, N. Alex.),:'rom loamoletostr. Tekb.
V0ZdUSh- Fl')ta; 13: 99-104 (1968)- 201OP- 24Dep. NTIS.
21physics; translationS 2120
26MN-34 29P NSA

Analysis of a Circular Cylindrical Shell
Subjected to Dynamic Loading, by
Yu. N. Alaksoyav, Ya. A. Limburg.
RUSSIAN, per, Samolet i Teldi VozcAush Flotat,
No 13, 1968, pp ITB--f-2O-.
CIA X-6896
7
Feb 69 374,2,3-7-

Imalytacal 21-lethod for DrAzzinining the Sorvim
LiUm of oil in in Lbgino,, by V. N, flikhomiMovo
No 16 lAtvJncyv. a ppe
RLUSIAN, porp Samolet-cat-m i Te)dmLka
Vazdushn 1 Ft ; i.. -No 196 6, pp - JLZ==.
A&I I W-2 6 9
sci/fuels and prcp;
nW 70

Calculating Flexu= and Std~)Jjity of
Rectan#i;ular and ftnrectanglaAar AnInotralitc,
Pjazes by tho Differensial DifformletT.
~10th0d,, IVY YU. P, POtTOVX III
Toklmika Voxab 0 Flato 1RIT. =10. is,
V~,,6 1 M4
A1V/r-T0j.1'-C-23-4(V1.70
P11! 71

Estimation of Stability of Elast.-*.c hloncircular
Conical and Cylindrical Orthogonal Crisingn,
by Yu. 11. Patrov. 21 pp.
ku-s"UrNNO perv Sawletostro ciniye i Tekhni1a
IJozdushnq.go clila,'71on --S,, 5-89,
- . -~17
AWR7r-TV-IIC--23;T6-67-"
sci/acronautics
fob 71

P14stic Mng idth Lminar Profils., bX
0- R- ICbWMDVWdyg V. B. Z)sulyr,. 9 pp,
EVS&[M,D perp s Takkmil,-a
vo I
0 no i no -~n
W IL7 IO]N 0 9 1 "91
't pip 161-IM007
scl/aem
fab 7i

Conversion of Saveral ComputtlationaL Algorithms
For DecreasIng the Length of the Word Folraat of
Control Cbmputers for Aircraft,, by I. N.
Koranot,, ct al, 5 pp -
RUSSIAN., per.~ Samoletostroy2Ejye i Tekhnika
VozdUshnogo Flota, No 14., 1 969_, pp 21-24-
AUVETDAIC-23-865-70
SePt 71

~ M M -'l,,.~l'l-.-'l"-'l.,-
ijT]
0.0
TY
Ji

TR ORLPOK Ti!59
k
INn4wicE or riq.,r, lanuigif T:Lwpl?, Oll THE, PLASTXdZ7
Or'' MST lls,~'AND -ALLOYS,
03100i, V. G'. RUSHMARMKOi, SlAki
&
'0
evi,
0

o" ~ 0" ~ ?I
! 0

V. T. 02ows
bi"katigation of tha takqqff,--7i=dp~g c*araotorliotias
j
horn` taksoff and Iztdii:~ (OWZ) 4et a-trorafts
pp.
RVSSXAN, ~SqmoUtostro oni o l' teJchnika vosdushno-go
sept 72

Detei%ination of Optimum Pariunetern of the Means Used to
Protoct the C=U)artments of an Aircraft, From Aerodynwdo
Hedt~:At Higb Speeds and During a Prolonged Flight,, by
Fal Gi~ Yasin'skiy,, 14 pp.
SAMOLMOSTROYMIMi I TEKM;M VOZDMEN(X;o FIMA, No 22,
-"i755-7P-
Feb

BjjlDta,, -ON THE
TIM --b
SURFAC
-R
In OF COMPRES9
1;, 17
VII
I ~Tr
i4v,
:0
20
~tk

Aircraft Navigation, by S. S. Fedchin.
RUSSIAN, bk V samoletovc,zlideniyo, 1966,
SSS pp.
NAS/NASA/TT F-S24 69
Sci-tlav
MaT 69 376,321

Smi-Aero
swb 69
393.,v2BD

_j 1-Indlilpz t~u Jcjajjtjj~y " - mal
j,rci)3)jj.,k of jLaojm, to
.A . i rawnaip
~IjtUUtjr,Tm~,p I)y Wo A* Aymm~mip L. 1, 3
et ale 9 pt.Ao
ULZVUL, xljrte i-~wocw.- Institubaimusnatiki i
a Avto-
191,66 3-8.
~;ci/lyahavoxial sci
feb 6 9 375f643

!bout Scm Basic Principles of Ccnstructing
Training Identificatim Syztemu, by
V. A. YAkUboVidI. 16 pp.
RIX-33.1ilij, rpL, ImsUA-ut Avtctnatiki
Sanmbudialishchives-va -zivtamti7
Mes U-y-e sisteiW, 1966, pp 9-20.
IM S-728
4137-69
july 69 384,299

Matrix Y*thod o-Ir Puttwn Rmoognit1cm w5d
Cortaln Froblemm In tho CwuAxuat'Um of
st&Mwdso bv Ve It, T2%kbtmns 9 Ippe
Russmulo
T
l*jzm- Slg~Aws 14001m. ~d-vo
IN-ALomk 1966,p py -63-59.
jOR/MD,/HT-23-15?,3-0

Cartalin Problem of OVU=m Fattwn ReacgnMonv
tDr 6. A. Mod"deve 9 ppo
RUSSLUJO PWIF 140sawo- lnv-tUqU~ LJJd
A 1.4
T--
M s flva b I2d-vO
Avtai
luw~p- 1,966-9 pp 60-W.
MRD/ig-23-1523-6?
Soi-Blect & Elect Engr
Jan 69

TaaabiM ftttorja hooog?dtian in J)DOIO&n
Spnool, bj A, D, Zakravsklyo N., Ro Toropav,
8 pp.
RMIAN9 per#
Taliwakhad3dow Samoobacftvu v
- - -- 9 A 1 Y. &VO
V pp 6V-720
1mvp-TD/JiT-2
T
Sol-Elect a Elect Enar
Jan 69 37D~871

glom Atopwto ce Pattmra Recognition vitik the
,4011(cutlcln Of MnVXbDld IMumto, by A. B.
Vm1binj, 9 pp-
Sm. IrxttlLt-i&. Avtomtlki I
per*
M-b
lbuAml I , PilAy-ollm -IilLr-tcm-
-101
F2D-sT.p3.ioh4.67
Scd-mectrmicz & Ln--c lbgr.
Sept 68 3660,034