SCIENTIFIC ABSTRACT SHMUTER, M.F. - SHMYGLEVSKIY, YU.D.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001549810012-0
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: August 23, 2000
• Sequence Number: 12
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

BIBIKOVA, V.A.; IL'INSKAYA. V.L.; KALUZHENOVA. Z.P.; MOROZOVA, I.V.;
SM4UTER It. F
_shik-Otrau.
Biology of fleas of the genus Xenopsylla ~in Sar, T
Zool. zhur. 42 no.7:1045-1051 163. (MIRA 17:2)
1. Central-Asian Research Anti-Plague Institute, Alma-Ata.

b I Fill ~GV A, V. A.; G,() FII;IJN,~ V A, A. 1. . [dec,! a,, -,,,I j ; Mu,.~:,L I ~,'NN -IKOV A, Z . P. ; MDR OZOV A,
1.1,1.; fu-TEFI, M.P.
Methods of studying the ab-andance of 'Lleas of the greater
.-erbil. Zool.zhur. 44 no.8*1214-1218 165.
(MIRA 18:11)
1. Sredneaziatskiy nauchric-~-4-ssledovatellski.,v protivochumnyy
institut., Alma-Ata.

-ACC.NR 5T4,Wr~6__
- AP700116 VRCE CODE: TJR/0439/65/044/008/1214/1218
AUTHOR: Bibi.kova, V. A.; Gorbunova'. A. 1. ; Maslennikova, Z. P. ; Morozova,
I. V. ; Shmuter, M. F. - -Schmuter, M. F.
ORG: Central Asian Antiplague Research Institute, Alma-Ata (Sredneaziatskiy
nauchno-issledovatellskiy protivochumnyy institut)
TITLE: Method of studying population density of fleas in Rhombomys opimus Licht,
SOURCE: Zooloticheskiy zhurnal, v. 44, no. 8, 1965, 1214-1218
TOPIC TAGS: flea, flea reproduction, flea migration, plague transmission,
disease vector, mole
ABSTRACT: A technique for total count of fleas found in the burrows of Rhombomys
opimus Licht. is described. The technique consists of trapping and counting ihe
--'aerating parasites after the animals are removed from the burrows. Due to a
relat,-.--1V stable migration and the reproduction rate of fleas, three samples suffice
for the total count. In practical terms, it means that all fleas present- in the burrowE
can be trapped during the 7-45 day period after the removal of the animals. The
total flea population in the burrows can be estimated on the basis of the relatively
Card 1 / 2 TJDC! 595- 775!59q. 323- 4 Rhnmhnmvs -

ACC NR- AP7001165
stab,le percentages obtained in sampling procedures. In view of the significant role
of fleas in transmission of plague, the importance of monitoring the flea populations
is stressed by the authors. Orig. art. has: 1 table. [Based on authors' abstract)
[WA-501
SUB CODE: .06/SUBM DATE: none/ORIG REF:, 006/~,
Card 2/2

SIAIRNOV, S.M.; TLEUGABYLOV, V.K.; SHOTER, M.F.; UZBEKOVA, B. R.
Epicutaneous imm-nization of subjects agaInst bruce2lDs-is with
a vzLceine from Brucella abortus strain 19. Zhur.mi~roblol.epid.
i immun. 32 no.1:51-54 Ja 161. (MIRA 14:6)
1. Iz Sredneaziatskogo protivochumnogo instituta Ministerstva
zdravookhraneniya SSSR. (BRUCELLDSIS)

BULIKANOV, A.A.; SHMUTER, S.L.
--------
Investigating electromechanical braking of the driving gear of
a milling machine. Stan.i instr. 33 no.12:21-24 D 162.
(MIRA 16: 1)
(Milling machines-Electric driting)

SHMUTER, S.L.
Specification of the technical characteristic and selection of
rated conditions in designing longitudinal milling machines.
Staii.i instr. 34 no.7:7-12 J1 163. (MIRA l6j9)
(Milling machines--Design and construction)

F,U! i tNOV, ',,,A,) --fl"MUTER , S~ L ~
system anr horrors of crograr. contrclied m~-chlne
.., -- I u -
(YT;;A I~Z-,)
Stan, -_i ln-sttr. 35 rlo.11:3-6 N 164. - r. I

SIMU"ILIFIR , 3 . L, .
Analysis of dynamic errore of program control-led miIIIIng machines.
st-an. i instr. 36 no.418-12 Ap 165. (IMIRA 18: 5)

SHMUTTER, A.V.
Bursitis in miners. Ortop.. travm. i protez. no.6:55-59 M-D 155.
(HLR&. 9:12)
1. Iz Gorskoy bollaitsy, Voroshilovgradskoy oblasti.
(BURSITIS
etiol. & clin. aspects, in miners)
(OCCUPATIONAL DISEASES
bursitis in miners, atiol. & clin. aspects)

A
0~-'IOVOY~ UL,"'IANYUK, A.A.
2. -LSS.1
L . K,:xakul Sheep
7. ~'-r-'LnciPIes in (ievelopin.- anti car-inp, for tne flock on state kaxakul farm.
CL
I zver. 5, 19521-.
9. Monthly List of.Russian Accessions, Library of Congress, January 1953, Unclassified.

SHISUTW, S.
Equestrian competitions. Voen. znan. 25 no.4:18-19 Ap 149.
(MIRA 12:12)
(Horeemanstlip)

BYCHKOV, N.P., kandidat tekhnicheskikh nauk; SHMLJYLOV, H.L., redaktor;
VOLCHOK, K.M., tekhnicheskiy redaktor
[Shipe of the maintenance fleet] Buda tekhnicheskogo flota. Lenin-:-
grad, Gos. lzd-vo vodnogo transporta, 19-54. 4Z4 p. (MM 9:6)
(Dredging machinery) (Excavating machinery)
(Ships)

DORKIDONTOV, Nikolay Konstantinovich, doktor tekhn. nauk, prof.;
LYSEVY10, Lavr Georgiyevich, kand. tekhn. nauk; PAVLOV,
Aleksandr Ivanovich, dots., kand. tekhn. nauk; TERMITIYEV,
Georgiy Borisovich, kand. tekhn. nauk; SIMUYLOV..-Nikola
Leonidovich, st. PrOpod. inzh.; Prinimal uchastiye RUMSOV,V.P.,
kand-.U-RTffi-.-na--a-j dots. 4 didLYAKov B.N. dots,., retsonzent; GRINBAUM,A. F..,
inzh.retsenzent,-VARETOV,P.C.,inz'h-.',i~etsenzent;ASM,V.V.,red.;VOLCHOK,
K.M., tekhn.red.
[Design and arrangement of ships for inland navigation]Kon-
struktsiia i ustroistvo sudov vnutrennego plavmiia. Pod ob-
shchei red. I-I.K.Dormidontova. Leningrad, Izd-vo "Rechnoi
transport," Pt.2. [Metal shipsll,;'etallicheskie suda. 1962.
271 p. (MIRA 15:12)
1. Kafedra arkhitektury i proyektirovaniya korablya Lenin-
gradskogo instituta vodnogo transporta (for Dormidontov,
Lysenko, Pavlov, Terentlyev, ShmtWlov, Kuznetsov).
(Naval architecture)
(Ships, Iron and steel)

AKOLIZIN, P.A.. doktor takhn.nauk; DANILEFKO, D.A., kand,takhn.nauk-;
KOLODEZNYY, B.A., iny-h.; KULAKOVj M.A., Imh - SHMM~OVICH I-Mi
inzh.
Prevention of hydrogen corrosion bjr means of hydrazine.
Teploenergetika 4 no.11:95 N '57. (MLU 10:10)
(Feed-water purification)

1-1 __ T .
,,~ _~ ~__ - ;I-
SHMUYLOVIGH, I.Kh., inzh.
Selection of a method of water treatment for power plants. Teplo-
energetika 4 no.12:52-54 D 157. (MLRA 10:11)
1. Lesenergo.
(Feed-water purification)

!!.' **.. 1, i ~ ~,: ~ !'!' ,kI- i I . I ! .'. 1:' '~ I. . I .~: I ! .:~.
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1'~. , , , . R
S t,, L t i. ,-)n , T ":: ~ " ; , '.f- , C. - , - I . . I !, - , I ",.
11 . I I ..I ., i -~ - I : r",'- . ...'o CMIRA 18;-10)

GROMOVAY V.V., inzh.; SERfUYIDVICH, L. Ya., inzh.
Tables of specific power ratings for light fixtures with
ineandescdnt lamps. Svetotekhnika 7 no-4:18-26 Ap 161.
(MIRA 14:6)
1. LO Gosudarstvennogo proyektnogo instituta "Tyazhpromelektrbpeyekt.,
(Electric light fixturesUbles., calculations, etc.)

ORECHKIN, D.B.; POPOVA, N.V.; FEDOROV, A.P.; SHMTIKO, O.F.; SHMUY'WVICH,
M.M.
Oxidation of paraffins in pilot plant units. KhimA tekh.topl.i
masel 5 no.7:16-18 Jl 160. (MIRA 13:7
(Oxidation)
(Paraffins)

ROZMSVIT, A.I., kandidat meditsinskikh nauk; SHKODINA, A.I.; SHHUYLOVICH, T.N.
Industrial accidents at the Odessa Ship Repair Yards. Ortop.travm. i
protez. 17 no.6:128-129 N-D 156. (MLRA 10:2)
1. Iz kliniki ortopedii (zavduyushchiy - professor H.L.Dmitriyev)
Odeaskogo meditainskogo instituta im. U.I.Pirogova (direktor -
professor I.Ya. Daynaka) I polikliniki No.2 (zaveduyushchiy Ya.S.
Sotnik) Chernomorvodedravotdela.
( ODESSA- -SHIPS -MA INTYNARC:g A11D RKPAIR)
(IDUSTRIAL ACCIDENTS)

EPSHTEYN, R.B.; FARBER, E.L.; GUTENEVA, L.Z.; SIZIUYLOVIGHt D.~.
Vanillin from sulfate liquors. Bum.prom. 37 no.1:20 Ja 1622.
I O-Mi 15: 1)
1. Uk-rainskiy nauchno-issledovatelisk-ly institut pishchevoy
promyshlennosti. (WoodFulp)
(Vanillin)

- -7- -t2v-7
.1 ~- 1 41 z~'Zt-' - t' ~ - - - : ~ ~ C~- -
GILIBO, M. P., SMMOVICH, Ya. M.,
Brain - Diseases
TwD cases of salvarsan encephalopathy; cure. Vest. ven. i derm. no. 21 Yjarch-April
1952
Monthly T,j5t of -Russian AccessLons, 4brary of Congress, August 1952. UNCLASSIFIED.

3ERM.AN, H.A.,knnd.med.nauk; KARLIN, M.I., knnd.med.nauk; SHMUYLOVICH, Ya.R.
vrach.
Toxiderma during treatment with sinestrol. Vest.derm. i ven. 12
no.1:77-78 Ja-F '58. (MIRA 11:4)
1. 13 Kozhno-vennrologicheskogo disnansera No.3, I.-ningrnd.
(SKIN-DISEASES) (ESTROGENS)

. . ~ ~ 1: - : ~ I , - . I ~ t -
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-ACC-N -(-)V)
i AP6034949 SOURCE CODE: UR/o146/66/oo9/oo5/oi16/0120
jAU71iai: Shmuylovich, Ye. G.
IORG. Ianingrad Institute for Aviation Instrument Construction (laningradskiy institut
laviatsionnogo prkborostroyanniya)
TITIE: A method for reducing the reaction of a gyroscopic compass to random
perturbations
SOURCE: IVUZ. Priborostroyeniye, v. 9, no. 5, 1966, i16-m
TOPIC TAGS: gyrocompass, metal friction, error minimization, ship navigation
ABSTRACT: The article reports the results of an investigation of the effects of
parameters of different types of rotation on the value of the error of a gyrocompass
in supports with dry friction, under conditions of the irregular rocking of a ship.
If the horizontal suspension of the gyroscope is placed in the diametral Plane of the
ship, the error, ok , of a gyroscopic compass, due to the presence of dry friction in
the axis of the compass ring, can be determined by the equation
H ~ (t) =M,+k sign [6 (1) +
where (t) is the healing angle.of the ship, which is a stationary random function of
time; MIL~r , and k constants; /5 (t), is the absolute rate of motion of the gyroscope
Card 1/2 UDC: 62-732.4

ACC NRt Ap6034949
witlh respect to the inner axis. It is shown mathematically in the article that the
use of a support capable of.different types of rotation can reduce the friction In the
i
support and permit a substantial decrease in the error of the gyroscope under
conditions of irregular perturbations. Ovig. art. has: II formulas.
SUB CODE: SUBM DAM *16Apr66/ ORIG REFj 004

SHMUYLOVICII. Tu.,inzh, (Omsk)
Utilizing the heat of motorayble engines for vulcanization
of tire tubes. Za rul. 16 no.10:13 0 '58. (MIRA 12,-l)
(Vulcanization)

-SHMYAKOVO A.M.
Feeding of sodium silicate by pneumatic tubes. Lit priozv. no.l:
36-37 Ja '61. iMBA 24:2)
(Sodium silicate) (Pneumatic-tube transportation)

SHMKOV., A. ~L
Automatic mold pouring. Lit. Proizv. n0.5-18-19 14Y 162.(bMU 16:3)
(Founding) (Automation)

SHRYAKOV, A. M.
-- -------- --- ---
Automatic positioning of the cores in foundry molds. Lit. proizv.
no.8:21 Ag 162. (Founding) (MA 15:11)

SHMYAKOV, A-M-___
Multiple disk 4-slinger head. Lit. proizv. no.2:12 F 163.
(KRA 16 s 3)
(Foundries-Equipment and supplies)

, W-rK, f, 1, FV , .,, 1 , r. ,* T ': r L 1, - .
. ~ ~ , . ".. I -k" I l - i k, ~ . .
of rh ti " ~-.clrrov tlu%-JrfC M~a " ~ FE g I t ~; I ~
'Zov.--ap. RSF-SF no, l.: i i~~j,-U' '62.
- poi. ~skop. .- I , - 4
il,',L,RA -,'-7 : I ~-I';
I

'~ . T ~! , - F M,A.
1 01-1.. -
1-:HT-rfG."LEV~ - ~; 1. fll,",~.i, i
M--~rphclo?,7 or %',je "7c-dc-r,-,r ~ntrusfon. 10'a , 2 P:, ; ".1~
- - I
-,. pol. Jskop, Sav..--~ap4 RSF,";R no,-!~-139-142 162.
,~ , 'A
.M--Tt -- -,-,
t

L 35071-65
ACCESSION NR.* AR5006368
10,400 is produced at -51C. Chains of vinylbutyl~e~ter.pre6minate iTi -the.struc_
ture of the copolymer, and transverse bon6s are present on . account of-tbe divinyl
chains. The copolymerization of vinylbutyl ester with divinyl does not occur -under.,.
the effect of phosphorus anhydride and ferric chloride. The polvvinvlethy! ester
is copolymerized with styrene (1:1) in the~presence of fer r i cchloride and in the f'
:ratio of 1:2 in the presence of the dinitrile-of azoisabutyric acid.. The copoly-,
.mers produced have a molecular weight of 56,000-76,000.and form-:films resistant.ta,
water and dilute solutions of-acids and-bases.:,Vinylbuty1:_ester is copolvm6rized--- i-~
with styrene in a 1: 1 ratio (FeC1 as' ca't*aly sit) and'l: 8:'r4f'- (BF-, as catai 0.
3 10 3- YP 2
~products with molecular weight of 2~ 000-50,000 are formed.~ The vinylphenyl-4ther'..,
is also copolymerized with styrene n ratios of 1:1 and 2:1 inthe presence of thei'".-.,
3 (as catalyst7, an&is also copolymerized with heating in ratios-.Of
esterate of BF
1:1, 1:2, and 2:1 at 100-1050C. Solid copolymers are obtained with molecular
weights of 48,500-92,000. Copolymers. of N-vinylacridonel6d Styrene are produced
i~i mass and in emasion; N-vinylacridone, styrene7,__~anlvinyl are produced in
emulsion and also N-vinylacridone, styrene, divinyl: and icrylonittile. . The prod__._,_..
ucts have molecular weights of 200,000-650,000. Of:the rubb6r-like materials most---.
plastic was the latter copolymer, containing N Vinylacridone, styrb-ne, divin'yl',, and-
acrylonitrile in the ratio 1:16:29:22. H-vinyldcridonexeduces the solifbility and
increases the hardness of the copolymers. S. Bass
Card
2/3

KISEISV, P., dispetcher; AFONSKIY, P.; GORBAVEV,
(g. Odessa); IONCSKU, Ion (Rumynskaya klarodnaya Respublika)
The fraternal international relations are growing stronger.
Sov. profsoiuzy 17 no.21:32-33 N 161. . (MIRA 14:10)
1. Makeyevskiy koksokhimicheskiy zavod (for Kiselev). 2. Pred-
sedatell Khartkovskogo oblastnogo komiteta. profsoyuza rabochik
mashinostroyeniya (for Afonskiy). 3. Redaktor zavodskoy gazety
11Za tekhnicheskiy progress" Orlovskogo zavoda imeni Medvedeva,
g. Orel (for Gorbanev).
(Trade unihns)

INYGANOVSKI'll vi. f.g.Odessa)
A seaman came ashore .... Sov. profsoiuzy 17 no.23:41-4.2 D 161.
(MIRA 14:1-9)
(Odessa-Community centers)
(Seamen)

AFANASIYEV, Ya. (g.Llvov); TKACH, M., instruktor; KACfVN, L.;
,SIMYGAROVSKIY V VOLKOVY A.; FRID, L. (g.Minsl:); PODLUZffl-.IYY, A.
-(g.Kiyev); YEVSTYUGIN, N.
Letters and correspondence. Sov. profsoiuzy 17 no.24:42-43 D 161.
(MIRA 14:12)
1. Krivorozhskiy gorodskoy komitat Kommunisticheskoy pa~-tii
Ukrainy (for Tkach). 2. Nestatnyy korrespondent zhurnala
"Sovetskiye profsoyuzyH g. Vitebsk (for Kachan). 3. Predsedatell
rabochego komiteta sovkhoza "Cherev',Kovskiy" Krasnoborskogo rayona$
Arkhangellskoy obl. (for Volkov). .4. Neshtatnyy korrespondent
zhurnala "Sovetskiye profsoytizy", Sverdlov-ikaya obl. (for
Yevstyugi-n),
(Community centers)
(Evening and continuation schools)

NEKAYEVJ, P. (st. Shakhunlya,, GorIkovskoy zheleznoy dorogi); BUROV, V.
(g.Kyzyl); SILIN, I., neshtatnyy instruktor; BORODIKO, I.
(g.Vorkuta); NAZAIROV, N. (g.Urallsk); MOSHKOV, P.;-
SHMYGANOVSKIY. V.
People talk, advise and criticize. Sov. profsoiuzy 18 RO~4:
26-27 F 162. NIRA 15:3)
1. Belgoi. skiy oblastnoy sovet profsoyuzov po Korochanskomu
rayonu (for Silin). 2. Neshtatnyy kor-espondent zhurnala
"Sovetskiye profsoy-uzy" (for-Borodlko,,,..9hmyganovskiy,).
3. Predsedatell sovata fotokluWVoloj~dskogo Dvortsa kulltury
zheleznodorozhnikov (for Moshkov)--
(~rade unions)

" ; .,- !- " !.'I , " I
.-.: I- - I i
I ':~~ -s Vi~,',! Overhaul, Ti -, 1,
1, - 0-,~ I
-j I L. -, " ,
, ;:
.l:-~!-.-.l';:j " 1, .1. o~f .

S WWGINJ I. I., (Postgraduate Student, All-Union Institute of Animal ffu5bandry)
The effect of terramycin and grisyn on blood factors in calves
Veterinariya vol. 30, no. 10, October 1961, PP 78

SHMYGIN, I.I., pspirant
Effect of terramycin and grisein on some blood indices in
calves. Veterinariia 38 no.lOs78-80 0 161. (KERA 16:2)
1. Vsesoyuznyy institut zhivotuohostva.
(Grisein) (Terramycin)"' (Veterinary hematology)

SHMYGIN, I.I., kand. biolog. nauk
Fertilizability of cows after the application of pregnant
mare's ser-am. Veterinariia 41 no.11:76-78 N 164.
(MIRA 18:11)
1. Vsesoyuznyy institut zhivotnovodstva.

SHMYGIXVSKIY, I., inzh.
Double-grid tubes. Wn.tekh- 3 no.4:53 AP '59. (MIRA 12:4)
(Electron tubes)

SHIMYGLEVOKIY? N. A., Cand Tech Sci -- "Increase ), ef-~ effec-
tive.,u-se of grain-harvesting combiines on lnolkwaa-at-tlie
0 il
automatic st,~'biliz cu.'the thresher in horizontal
position." Ordzhonikidze, 1961. (Min of Agri Uk-3SR. Ukrainian
Acad of Agr~ Sci) (KL, B-61, 252)
- 341 -

st. p-repodavatell; B:-;DRkK.
F aaricu- tural machinery'
fkh mashin.
r knlz~inoe izd-vo. 1961.

SW,YGLEVSKIY, Nikolay Aleksandrovich; BEDHAK, T.V.., red.
(Operating the hydraulic syl3tems of tractors] Ekspluata-
tsiia gidrosistem traktorov. Ordzhonikidze., Severo-
Osetinskoe knizhnoe izd-vo, 1960. 7/+ p, (MIRA 18-3)

'01. D., P. 1. ~m(l K'AT,'JIVA, 0. N.
"Certain Froblems of' Gas Dynamics" a paper presented at the Conference on. Methods
of Devetopment of Soviet Mathematical Machine-Building and Instrunient-Ruilding,
12-17 14arch
Translation No. 5'./;~_,, 8 Cct 56

I. . . . . .I --- - . I I
SHMYGLEVSKIY, Yu. D. Cand Phys-Math Sci -- (diss) *Variationgo problem of the
gas dynamics of axially- symmetrioAlupersonic currents.' Mos, 1957a Cover, 4 pp
20 cm. (Acad Sci USSR. Mnth Inst im V. A. Steklov), 110 copies (KL, 24-57, 115)
-9-

"'al
- clii;~~-on of axJs-syr_vietrJcaI L-as flu.-is Jn the ne-if7hiho,irhood
of a 'ureak in the 5-eneratrix of solids of revollition."
Two methods have been develooed for calcnlating, axis -syruretrical s1loersonic
~-as flo,.-!s in the ne4_'vhbourhood of a break of th,~ generatrix: of solids of revolu-
tion. T lie IIV~,Zt4 ~a.Lled flo,,Ts are t1iree-dimensfona- 1 ones wha-ch 13re analogous to
the Clo-u of 'saver. z3clution of 'the gas dynamics ecmations are found in the form.
of :)o,.,Ter series', the 'lirst coeff Lcients of which repres~_nt 'the flows of
Whilst the sul~seqiient ones are correct-ions takint: into account the axial s.-,imetr,,-
of the I'low. The f-4rst described method cermits determininF the magan-itude of
the soeed co!,vonents in an-,.- -,-."oj-rt of the --one of the bend where the anEle chanres.
irie second m-ethod 'rives the macnitude of the anFle of perturbations, the inclina-
,.-_n anf-le of the soeed ami the coordinates directi,-' ~'Or an:.- c~,aracterilstic of
the zor~e of I-endinr ihere 'the angle chanE-es. These values are recessar "Or cal-
culatinF the zone located ~e:,,ond the zone under -consideration.
(.T~;rst :.),lbl4shed 1950).
of Theoretical Wark on Aerod_,,,,n.c-,iic.s, OluoronE:iz, 1957, 3,000 copies,
~;entral "Lero-Hydrodmamics Inst. imeni Prof. 1". Ye. Zhudovsk-i,,,,.

.r,1Y6___1_E0r\
PHASE I BOOK EXPLOITATION 823
-Tsentral'nyy aero-gidrodinamich eskiy institut
Sbornik teoret~icheskikh rabot po aerodinamike (Collection of
Theoretical Papers in Aerodynamics) Moscow, Oborongiz, 1957.
509 p. 3,000 copies printed.
Ed.: Ushakov, B.A.
PURPOSE: This collection assembles &number 6f scientific reports,
on theoretical aerodynamics, first printed in various publications
between 1947 and 1952, and intended for research workers in ad-
vanced aerodynamics.
COVERAGE: The collection contains 26 papers on theoretical aero-
dynamics, published by the Tsentral'nyy Aero-gidrodinamicheskiy
Institut imeni Professora N.Ye. Zhukovskogo (Central Aero-hydro-
dynamic Institute imeni Professor N.Ye. Zhukovskiy), first
Card- l/ 33-------

Collection of Theoretical Papers (Cont.) 823
printed for limit 'ed distribution in various publications duriP3
the period 1947 to 1952. These papers -#ere of course completed
a considerable time prior to the date of publication. -The papers
presented in this collection may be divided into several groups.
The reports of the first group deal with methods of solution of
two-dimensional subsonic pr6blems for the case of adiabatic gas
flow (A.A. Nikol'skiy, B.M. Kiselev) and present several exact
solutions of the equation of three-dimenaional gas flows (A.A.
Nikol'skiy). The reports of the second group are concerned with
the study of supersonic gas flow around bodies of revolution.
Ducted bodies having minimum drag are considered (A.A. Nikol'skiy);
the relationship between the shock-wave curvature and the surface
of the ducted body is studied (A.A. Dorodnitsyn). The charac-
teristics of supersonic flow near sharp trailing edges are de-
scribed (A.A. Nikol'skiy), a general analysis of several cases
of axially symmetrical flows is made (A.A. Dorodnitsyn), and a
specific calculation in the neighborhood of the break in the
Card 2/33

Collection of Theoretical Papers (Cont.) 823
generatrix of the body of revolution is given (Yu.D. Shmyglevskiy)-.
The third group includes a report by A.A. Dorodnitsyn on a method
of calculating the pressure distribution on bodies of revolution.
at zero angle of attack and an extension of this report, the
paper by V.V. Sychev on bodies of revolution at an angle of attack.
The papers in the fourth group include reports on the boundary
layer and heat transfer. The investigations of A.A. Dorodnitsyn
on the theory of a laminar bouiidary layer in a compressible gas
and the investigations of V.V. Struminskiy on the theory of the
three-dimensional boundary layer on a slipping wing are presented.
The reports of I.N. Sokolova concern problems of temperature of a
plate and of a conetaking radiation into account. This group al-
so includes the investigations of V.V. Struminskiy on the theory
of the unsteady boundary layer. The reports of the fifth group
deal with problems concerning wing theory; methods of calculating
the circulation around a sweptback wing in subsonic flow (V.V.
Struminskiy and N.K. Lebed') and along wings of small aspect ratio
(P.I. Chushkin and G.A. Kolesnikov) are presented, as are also
Card 3/33

Collection of Theoretical Papers (Cont.) 823
papers on supersonic flow around cruciform wings and ailerons
(V.M. Shurygin). In the reports of the sixth group general pro-
blems are treated which are associated with the theory of com-
pressors (L.A. Simonov); supersonic flow around a cascade is con-
sidered by V.V. Keldysh, and the total-pressure losses in the pres-
sure discontinuities ahead of the cascade are disctAssed by G.I.
Tanganov.
TABLE OF CONTENTS:
Foreword
3
Nikol'skiy, A.A. Variational Equations of Two-dimensional
Adiabatic Gas Flows 5
The report, first published in 1948, gives a method of in-
vestigating two-dimensional adiabatic gas flows in the vici-
nity of given flows. The variational equations of motion of
a gas in the flow plane and the subsequent transformation to the
Card 4/33

Collection of Theoretical Papers (Cont.) 823
variables of the hodograph plane permits reducing the pr(*-
lam.. to the investigation of the solutions of the linear
partial differential equation of the second order common for
all cases under simple boundary conditions. The report is
divided into the following sections: 1. Derivation of equa-
tions; 2. Boundary-value problems. The report contains4
figures. There are 2 Soviet references.
Kiselev, B.M. Two-dimensional Subsonic Gas Flow Around Bodies of a
Given Form
The report, first published in 1952, gives a method for cal-
culattng the two-dimensional subsonic gas flow around bodies
of a given form. A first approximation may be used with a
high degree of accuracy. The report is divided into the fol-
lowing sections: Introduction; I. Mass-flow functions; 2.
Mass-flow functions in a complex form, a generalization of
Chaplygin's formula; 3. Canonical form of equations of motion;
Card 5/33

Collection of Theoretical Papers (Cont.) 823
4. Approximate method of solution of the equations; 5. Flow
around a circular cylinder; 6. Flow around a profile of ar-
bitrary form; 7. Another method of constructing the solution.
The report contains 10 figures and 3 tibles. There are 5 ref-
erences, of which 4 are Soviet and I German.
Nikol'skiy, A.A. Several Exact Solutions of Equations of Three-
dimensional Gas Flows 27
This report was first published in 1949. A class of three-
dimensional supersonic adiabatic gas flows is foundeach of
which is represented by a curve in the velocity-hodograph
space. These flows are a generalization for Me case of-the
space of known Prandtl-Mayer flows, and each of them may be
considered as the result of an undisturbed flow around a
solid wall, representing the developed surface. 'The results
of this paper may*be applied to calculations of wings of'fi-
nite span in supersonic gas flow. The report is divided into
Card 6/33

Collection of Theoretical Papers (Cont.) 823
the following sections: 1. Flow characteristics; 2. Flow
around a solid wall. The report contains 7 figures. There are
no references.
Nikol'skiy, A.A. Generalization of Riemann Waves to Include Three-
dimensional Case 34
This report was first published in 1949. Various three-di-
mensional adiabatic unsteady gas motions are sought in which
surfaces of constant pressure are simultaneously surfaces of
constant velocity vector. These surfaces are found to be
planes which remain parallel and move with constant velocity..
Special cases of the motions considered are one-dimensional
unsteady Riemann flows (Riemann waves), two-dimentional super-
sonic Prandtl-Mayer flows (which are steady flows), and three-
dimensional steady gas flows, the form of which degenerates in-
to a line in the velocity-hodograph space. The report contains
2 figures. There is 1 Soviet reference.
Card 7/33

Collection of Theoretical Papers (Cont.) 823
Nikol'skiy, A.A. Conical Axially Sy-,metrical Supersonic Rare-
faction Gas Flows 43
This report was first published in 1949. A class of axially
symmetrical conical gas flows is found in which an undisturbed
translational supersonic flow, starting from a certain Mach
cone with its apex on the axis of symmetry, is continually
rarefied, Each of these flows may be regarded as the result
of an undisturbed supersonic flow around a certain body of re-
volution representing a semi-infinite cylinder which, starting
from a certain cross section, gradually contracts. To any Mach
number (larger than one) of the appro'ach flow there corresponds
an infinite single-parameter family of such flows. The results
of this report may be useful in the design of the rear parts of
bodies of revolution intended for flight at supersonic velo-
cities (of fuselages, missiles, jet engines, etc.) The report
contains an Appendix and 15 figures. There is I German refer-
ence.
Card 9/33

Collection of Theoretical Papers (Cont.) 823
Nikol'skiy, A.A. Ducted Bodies of Revolution Having Minimum
External W-ve Drag in Supersonic Flow 56
This report was first published in 1950. Within the framework
of the linear theory, the problem of finding the shape of duct-
ed bodies of revolution having minimum external drag has been
solved. Simple explicit formulae are o 'btained for the drag of
bodies having miniuram drag. it is shown that within the range
of body parameters of interest from the practical viewpoint, a
change in the shape of the body does'not lead to a significant
change in drag if two initial sections of the body remain constant,
and that therefore the formula obtained for drag may be taken as an
approximation for a general drag law. All investigations were
carried out fcr the calculated regime of passage of a stream
through a duct, that is, for the case where internal processes
do not affect the external flow around the body, The report is
divided into the following sections! 1. Statement of problem;
2. Derivation of basic relationships; 3. Case where two sections
Card 10/33

Collection of Theoretical Papers (Cont.) 823
of the outer surface of a body and the distances between them
are given; 4. Some properties of ducted bodies of revolution
having minimum drag. The report contains 5 figures. There is
1 Soviet reference.
Dorodnitsyn, A.A. Dependence of the Curvaturr of the Compression
Shock Line on the Outer Surface Curvature of a Ducted Body of Re-
volution
This report was first published in 1949. The relations are
derived between the curvature of the line of a compression
shock and the curvature of a meridional cross section of a
ducted body of revolution. The relationship found permits
construction of the element of the line of the compression
shock near the leading edge, which is necessary for calcula-
ting pressure distribution of the outer surface of the body
of revolution. The report contains 2 figures. There is 1
Soviet reference.
64
Card 11/33

Collection cETheoretical Papers (Cont.) 823
Nikol'skiy, A.A. Gas Flows Near Sharp Trailing Edges of Bodies
of Revolution 74
This report was first published in 1949. Gas flows in the vi-
cinity of sharp trailing edges of bodies of revolution are in-
vestigated. It is demonstrated that, if the solid angle formed
by the body surface on the trailing edge is not equal to zero,
there always exists a certain region near the trailing edge in
which the velocity is subsonic. This applies, in particular,
to cases of gas flows around bodies of revolution at super-
critical Mach numbers of the approach flow (a flow with a lo-
cal supersonic zone) and at approach-flow Mach numbers larger
than one. The report contains 4 figures. There is 1 Soviet
reference.
Dorodnitsyn, A.A. Some Cases of Axially Symmetrical Supersonic
Gas Flows 77
This report was first published in 1950. Derivation of the ca-
nonical system of equations for axially symmetrical supersonic __gas
flows is given and methods of solving this system are presented.
Card 12/33

Collection of Theoretical Papers (Cont.) 823
As an example, the author analyzes the case of a flow in
the vicinity of abteak in the geneatfix df a . body of revolu-
tion which is a generalization of the known plane-parallel flow
around a corner. The report is divided into the following sec-
tions: 1. Equations of axially symmetrical flows in terms of
characteristic variables; 2. Solution of system when initial
values on two characteristics are given; 3. Other applications
of equations in terms of characteristic variables; 4. Equi-
librium flow around a corner. The report contains 7 figures.
There are 2 references, of which 1 is Soviet and I English.
Shmyglevskiv, Yu.D. Calculation of Axially Symmetrical Super-
sonic Gas Flows in the Vicinity of a Break in the Generatrix
of a Body of Revolution 89
In this report, first published in 1950, two methods are de-
veloped for calculating axially symmetrical suDersonic gas
flows in the vicinity of a break in the generatrix of a
body of revolution. The flows considered are three-dimen-
Card 13/33

Collection of Theoretical Papers (Cont.) 823
sional flows, analogous to Mayer's flow. The solutions of the
gas-dynamic aquations are found in the form of power series, the
first coefficients of which represent Mayer's flow while the sub-
sequent ones.are corrections for'the axial symmetry of the flow.
The first calculation method permits determination of the magni-
tudes of the velocity components At any point of the angle zone.
The second method gives the magnitudes of the angle of pertur-
bations, of the angle of inclination of velocity and of the
coordinates directly on any characteristic of the angle zone.
These quantities are necessary for calculation ol the zone lo-
cated beyond the zone considered. The report is divided into the
following sections: Introduction; 1. Flow in the zone around a
break in the generatrix; 2. Calculation of flow in the zone a-
round the break in the generatrix in terms of characteristic co-
ordinates; Appendix, The report contains 9 figures and 24 tables.
There are no references.
Card 14/33

-7:7
Q4; 'M
NEXOTORYE VA.
zovol PERAM Ii
-.7t
Zvvx"qVYKH,TEC
P~ikl M
Z06. In Ruset"..,S
g 5 yqa'm'-tca- 04 symme
a d
Tho'study

124-58-9-9624
Translation.from: Referativnyy zhurnal, Mekhanika, 1958, Nr 9, p 23 (USSR)
AUTHORS:,- Katskova, 0. N. , ShmygLey_-,~,
TITLE: Axisymmetric Supersonic Flow of a Freely Expanding Gas With
a Plane Transition Surface (Tables) [ Osesimmetrichnoye
sverkhzvuko%,oye techeniye svobodno rasshiryayushchegosya
gaza s ploskoy perekhodnoy poverkhnostlyu (tablitsy)]
PERIODICAL: Vychisl. matematika, Nr 2, 1957, pp 45-89
ABSTRACT: Calculation of an axisymmetric supersonic irrotational flow
of a freely expanding gas with a plane transitional (sonic) surface.
The problem is examined in the coordinates z, X. where z
is constant along the streamlines and stant along the
. 4nis con
characteristics of the secondfamily the vicinity of the
transition surface the solution is sought in the form of series
according to powers of X. A system of three ordinary
differential equations is obtained for the coefficients of these
series. The system is reduced to a third-order equation,
the solution of which is tabulated. The remainder of the flow
is constructed according to the method of characteristics.
Card 1/2 Tables are given for the parameters of the flow; the tables

124 - 58-9
Axisymmetric Supersonic Flow of a Freely Expanding Gas (cont. )
are computed for four values of the ratio of the specific heats 4 (K= 1, 14000,
Is 33000, 1. 40000, and 1. 66667). The tables contain the values of the Mach
,ingle, the angles of inclination of the velocities, the cartesian coordinates
and the pressure integrals at the points of intersection of the streamlines and
the characteristics of the second family. The tables can be used for the con-
struction of axisymmetric nozzles for jet propulsors cut off at the critical
section,
P. P. Koryakov
1. Gas flow--~Iathematical analysis 2. Supersonic flow--~Iathematical analysis
3. DiffLerential equations--Applications
Card Z/?_

SOV/124-59-10-li477
Translation fromg Referativnyy zhurnal, Mekhanika, 1959, No. 10, p. 60 (USSR)
AUTHOR: Shmyglevskiy, Yu. D.
TITLE-, The Calculation of Axisymmetric Supersonic Gas Flowlin the Vicinity
of a Salient Point in the Generatrix of a Body of Revolution
PERIODICAL.- Sb. teor, rabot po aerodinamike. Moscow, Oborongiz, 1957, pp. 89-115
TM~ A method Is given for calculating axlsymmetric supersonic potential
gas flows in the vicinity of a salient point of the rotation body generatrix.
The discussed three-dimensional flows are analogous to the Prandtl-Mayer flow.
Each required J-function dependent on,cert5,ln variables is represented as a
power series: i (~' 0 % + ?1' 0 + TZ ~)
The coeffIcients ?Kof such series can be determined gradually from the recurrent
system of the ordinary differential equations. Two variants of the calculation
method are presented: 1) the polar coordinates 0 , r are substituted for the
variables respectively; the system pole is the salient point, 2) the
variables represent characteristic coordinates; ; is constant along the
Card 1.12

SOV/124-59-10-11477
The Calculation of Axisymmetric Supersonic Gas Flow in the Vicinity of a Salient
Point in the Generatrix of a Body of Revolution
characteristics starting from the salient point, and -q is constant along the
characteristics of the other family. The zero coefficients of the series
correspond to the Prandtl-Mayer flow, but the following coefficients are
axisymmetrical corrections. In both variants of the calculation method the
formulations ~re obtained in quadratures for the first and second series
coefficlents. The arbitrary constants in these formulae are determined from
the Imown course along the first characteristic of the bundle starting from
fAhe salient point. For instance, two special cases are discussed-, a) flow'
around a rotation-body having a conic nose section and a salient point in the
gener-atrix, b) flow around a semi-infinite ciroular cylinder having a salient
po.int in the generatrix in its taill section, Detailed tables were computed for
a series of Mach-number values of the incident flow and also angles of the nose
sectiop, for plotting the flow in the zone enveloping the solid angle-,
P. I. Chushkin
Card 2/2
A

AUTHORs Shmyglsvskiy, Yu.D. (moscorr) 40-21-2-7/22
TITLE: 9ome Variation Problems of the ma Dynamics of Axialsymmetric
Supersonic Flows (Nekotoryyevariatsionny5ezadachi gazovoy di-
namiki osesirametrichnirkh sverkhzvukovykh techeniy)
1:
PERIODICAL: Prikladnaya Matematika i liekhanika,1957, Vol 21, Nr 2,
PP 195-206 (USSR)
ABSTRAM The author considers trio problemst 1. For an axialsymmetric
flow around a body of revolution let be known a characte-
ristic of one of the real families of characteristics. The ge-
nerating line of the body which caus--s the smallest wave re-
sistance has to be determined. 2. Determination of the best
form of supersonic exhaust nozzles. A detailed solution is
given only for the first problem. The author uses the control
surface (see Nikollskiy [aef 1j) and reduces the problem to
a degenerated variation problem which then is treated in de-
tail. There are 6 references, 5 of which are Soviet, and
1 German.
SUBMITTEDs November 12, 1956
AVAILABLE: Library of Congress
Card 1/1 1. Bodies of revolution--Supersonic flew 2. N*zzles-Dotervinatim
3. Gas dynamics

- Ax i a, Fir'-w-
as ;vnam-c-
,arll r3
dLosertation deferlded Cur the de,,-ree -f Cand. of 11hys-1.1-nUi Sci. aL the Inst. of
i4atii. Lm V. A. Ste?.Iov,
DeCenge c-f' Diasertati(-nij (Jari-Jul- L"I"57)
Section of Physical Mitit"n. ScL.
lest - A',,,' S'S'z",R, -27 , I,

AUTHOR:
TITLE:
PERIODICAL:
1 ABSTRACT:
Card 1/2
PA - 3131
A Variation Problem of the Gas Dynamics of the Axially-Symmetric
Supersonic Flows.
(Variatsionnaya zadacha gazodinamiki osesimmetrichnykh sverkhzyu-
kovykh techeniy. Russian).
Doklady Akademii Nauk SSSR, 1957, Vol 113, Nr 3, PP 52o - 522
(U.S.S R.)
Receiy;d: 6 / 10,57 Reviewed: 7 / 1957
The present paper is supposed to determine the shape of a body of
rotation with the lowest wave resistance in a supersonic flow and
the shape of a nozzle with the lowest losses. A diagram shows the
generatrix of the rotation body, the assumed characteristic of the
first family, and the required characteristic of the second family.
By means of the method by A.A. Nikollskiy, the problem investigated
here can be formulated for the functions on the assumed characteri-
stic of the first family.
At first the denotations used here are explained. The variation prob-
lem resulting in the vortex-free casd is exactly given and the cor-
.L
responding equations are written down explicitly. This problem is de-
generated, because the derivations of the functions are contained
linearly; it may be solved by means of the method by D.E. Okhotsimskiy,
Prikl. mat. i mekh., Vol lo, p 251 (1946). The solution furnishes the
following results:

9(6) SOV/112-59-2-3461
Translation from- Referativnyy zhurnal, Elektrotekhnika, 1959, Nr 2, p 175 (USSR)
AUTHOR: Shmyglevskiy, Yu. D_
TITLE: Use of Electron Computers for Engineering Calculations
(Primeneniye elektronnykh vyc hi slit el'nykh mashin dlya inzhenernykh raschetov)
PERIODICAL- V sb.: Mekhaniz. ucheta i vychisl. rabot M.-L. , Mashgiz, 1958,
pp 19 -26
ABSTRACT: Structural principI es of digital computers are briefly discussed,
using the BESM computer as an example. Five examples of engineering
calculations performed on the BESM computer are cited: (1) solution of
problems of the theory of maximum equilibrium of soils by the method of
characteristics; (2) calculating supersonic streams; (3) stability of long-
distance electric transmission lines with an intermediate synchronous
condenser determined by integrating a set of nonlinear differential eq-1ations;
specifically, the Kuybyshev -Moscow line; (4) determining the aerodynamic
Card 112

SOV/112-59-?-346i
Use of Electron Computers for Engineering Calculations
characteristics of profiles and solids of revolution in a subsonic air stream,
using the method of integral relations; (5) calculating the terrain maps by the
iteration method. The need for specialized computers in solving this type of
problem is noted.
Yu. M. Shch.
Card Z/?

AUTHOR: Yu.D. (!"'oscow) 40-22-.2-18/21
Shmyglevskiy
,
TITLE: On Supersonic Profiles Possessing a Minimum Resistance (0
sverkhzvukovykh profilyakh, imeyushchikh minimallnoye so-orotIvie-
niye)
PERIODICAL% Prikladnaya matematike, i mekhanika,1958,Vol 22,Nr 2.
pp 269-273 (USSR)
AL,5TRACT: For a profile in supersonic flow of a gas that form is sought
for which the impact wave resistance is a minimum. It is
assumed, that there exists a uniform gas flow with a velocity
constant at infinity in parallel with the X-axis. Furthermore
there are assumed two points A and B through which the sought
profile is to pass. The point A is to be the starting point of
the profile from which a shock wave originates which in certain
cases may degenerate into a characteristic of the flowing gas.
After setting up the integral formulas for the forces acting on
the profile, the problem is formulated as a variational problam.
For the solution the method of the Lagrange multiplier is
applied.
The numerical evaluation shows'that the profile which possesses
a minimum impact wave resistanoe in the present cases is
2 practically identical with a wedge. The profile consists of two
Card 1/

On Su-personi-. Profiles Possessing a Minimum Resistance 40-22-2-18/21
rectilinear parts to which a relatively small curvilinear part
is attached. The results of the evaluation are represeniCed 'Lrk
two tables and several diagrams.
Thers are 4 fftE~uresq 2 tables, and 2 Soviet references.
SUBIIITTED-. September 239 1957
i. Ga2 flow-Mathemat4 cal anal~rsis 2. "~upe-sonio flow---~-'-athe:i,.atic-a'I
ara -, -,s -4
Card 2/2

SHMYGLEVSKIY, Yu.D.
Using electronic calculating machines in engineering calculations.
[Izd.] WHITORASH 44:19-26 '58. (MIRAL 11:9)
(Electronic calculating machines) (Engineering)

'5 6
soV~-o-122-5-,-'/
Yu. D.
Su--con-,
of t',e -C
0;.
F L: o f oserim7netrichn-1:h
0 no'zoto--,yi,~h
'is 's :1,J
t
'Cr r. v C
T--
--re deterriined
first family AC and by tne
f*ztjc of t
t i of tl-.o body of rotation round v.,hich
Satisfy a
---'n4Ch is given here.
4C b -
stem of ewiations
written down.
.-_o fo r flow fu,,-,ctiori a relLAion is
A --short re~;ort ic ma(Je on the course of calculation
-L,-d or. oc):ae boun,,'--:.,y conalitions. Finally, the following
co-nc,lu~74o-ns to be drawwr: 1) in an z.~4a!'Y-
cuj.~el,l,.On~c round Ll body of rotation
R of ~'- e
of t!:-.,? rLdius of curvature U-1

t-.p- A xi,~.l ly-Sy:me t~ ri c SuL-r 1-:~ on i CSOV/2o-122-5-9/tJ6
of a
4
to
borl- the Point A le--ds
a de=ase cf t':Le deri-vatives da/ds and d-Vds on an
,-E:zu.-ied AC. The si-jns have here
U--
~~-'~-n -into account. a denotes the Lach
U i,~ J1 and 4- the angle of inclination of
_ y -.,j 4
vv,--,c~t Ith res,)ect to the axis of the -flow. 2) In an
supersonic flow of n bo,--'y of
c r e:~ s e
1
,, of t~e radius of curv,--ture
Ft of t~--e ~'B of the body of rotation at the
A causes an incr~----ese of' t1l,e r,-'.dius of c,,,.rvature Rb
o-f t',-.c- lii~e of tic- chock ,-,,ave CE at the point C if A
~~-A C conn"cted with ea-h other by a character ist i c
of Thp-re are 11 fi,-ure and 1 Soviet
reference.
ASSCC-L--L--Pl;.)',l: V:,-c.'~i.-litelln-y tsentr Akademii nauk SSSR (Com-putation
11 -
Certer of t'-Ie Academy of Sciences USSFL)

AUTHORS. Lanido,,K.S., and Rkov.,E.S. SOT/42-14-1-27/27
TITIA. Publications on Applied tatlysis anI Numerical M.th.matic.-
Isilmly. po p,ikl&d-- --its- I ~Y-111-lit-l'tay
PMCI)ICAL, U:p:ri isst-tichoskikh --,,-,1959,Vol 14,Xr 1,pp 261-265(USSR)
ABSTRACTO I stated th at in the USSR there exists no periodical on
orical "th .. tics and similar domain., Th. v ... to of 1h
do-1.4 ohi&sfly appear in the seriv. "publications ca Appliod-zol"..
and N-. 'I I VAth.a&tjc*- (BPAVU) and In single coll4ut.d
voluse.o. The ..rise 3PITX began 1- 1955 ad nt 11 n3w It
con t&Icad the following "cographiose 1. C.S.Salakhow
of Seriam"i 2. A.W.Khovanakiy -Application of Continued Fractions
In the Approximat. Analy.i.-I 3. V.3.Ryab.n-kly, A.F.Filipp.-
.at , t, U_ - -
&b, I of Difference Equationim; T. 9 Vol I "a"'
gramewl S. SoMplikollskLy -Quadrature ?a "u1&o1iq:11V.A.Xrt;.,
Arith-sto D.,ic.. of ll.at"ni. Digit Apprat~-j 77._K77
Tcmb- , -Ma ... t" Method In Applied Wh-tic.., a.-W.T.
E~~ G.S.Noslyokol. I.P.Trifonov, X.R.Shurs-Bura -B-yaEsm
. t=d--3-.Vy-r.Fr-e . - '
Thor. appeared the following collected volumems -Numerical
--N&ti -;;tics and Computing ?.chat..- (VMVT) too 1953."Numseric.1
Whe"tins' (TM) since 1957. and 'Contputing T.:bmia.- (VT)
3a. Until now, two vol"os of VXVT appeared with contributili:_
1 19
of T.A.DitkIZ, L.A.Lyumtemik, A
Sho2s, ra, A.L.fsorova. G.;1,1h0vaasX Y,
vZ71the P-M-Nared -or Yx coutsimal contrit-utiumv
oTL.A.LZustemik, Tu.T.Torob-y.,, T..,L*Volko,, V.K.S.u'lly
n ILLY. SP-
,A.I.Taorcr::
Wulf, _121
IR SVur.- I t--.
so,
To 7=71.-P~ S.M
toki , - 2,1~rt :Dr,3do A,G .......
v, 2.1 sic-tawrove,.iy. The-7-trat volu-m-&-o-M con a a
to
Ishl
. Zel~
but 0, PZ.3ht bakay, ?.Y.*jLyorov, F.P.Golorlettkov.
WWR
T..A.Tolkov, L.T.Grolovb N.Y&. "t "in, O.T. Gv ~y_ -.3
ITU-0ra-v T-IM-.0.0'.
f;;md..' ollc'*d
.:dit
.:d Ih:.,
0!: kly
.4u.sti -it I Me I....
toorli "t-ticho.k1kh va.blm-) with o.tribution. of T..T..
lmsilo,skiy. X.T&.Lk..hskiy, TLL.A.Shroyd.r, Z A
r9, v.s.uiaskiy, M.r..a
L
C&sd 3,13
if

10 (2)
AUTHOR: Shmyglevskiy, Yu. D. SOV/20-126-5-12/69
TITLE: On Bodies of Rotation Having Minimum Resistance at Supersonic
Velocities (0 telakh vrashcheniya, imeyushchikh minimallnoye
soprotivleniye na sverkhzvukovykh skorostyakh)
PERIODICAL: Doklady Akademii nauk SSSR, 1959, Vol 126, 11r 5, PP 958 - 960
(USSR)
ABSTRACT: The following problem is set: The velocity w 00 of the gas flow
striking contour AB and points A and B is given. The author in-
vestigates the case in which a shock wavo AC appears in addition;
BC is assumed to be the characteristic of the second type andCD
that of the first type. The problem is dealt with according to
reference 1 . The search for contour AB of the rotation body with
minimum resistance can now be regarded as a problem of variation.
The constants w'MP r r., Xmx,-x are given and the
A.$ A
C function CM is desired, which realizes the extreme
B value of is given by
It, Y' 1 $
-77- (W + -)-a(a) cost- 1 inasin(~-a dly
A 4X 00 Woo
Card 1/2 T=TA

KATSKOVA, OlIga Nikiforovna; SEMYGUVSKIY, Yu,.D., otv.red.;YAKOVKIN,
M.V., red.; KORKINA, !-.!-.--,--tekhn.red.
[Description of the programming system of the BESH-1 computer]
Opisanie sistemy komand elektronnoi vychislitellnoi mashiny
BESK-I. Moskva, Vychislitellnyi teentr M SSSR, 1960. 70 p.
(MIELA 14: 1)
(Electronic digital computers)
(Programming (Electronic computers))

87794
~S/040/60/024/005/017/028
C111/C222
AUTHOR: Shmyalevskjy,-jua, (Moscow)
TITLE: On a Class of Bodies of Rotation With a Minimal Wave Resistance
PERIODICAL: Prikladnaya matematika i mekhanika, 1960, Vol.24, No.5,
pp.923-926
TEXT: The author seeks the generating line AB (figure 1) of a body of
r
A
rotation for which, for given er 00 , rAand rBthe wave resistance is
Card 1/5

S/040/60/024725/017/028
C111/C222
On a Class of Bodies of Rotation With a Minimal Wave Resistance
minimal. It is assumed ihat the skock -rave AC is an adjoint one; BC is
the characteristic line of the second family2 CD is the characteristic
line of the first family. It is shown that the determination of AB leads
to a variation problem which in general has no classical solution. The
classical solution eiists only if w rA rB , where X = x -x
a) ' T ' T B A
satisfy very special relations (cf.(Ref-4)). The figure 3 shows for
several Mach numbers the results of the calculation of some possible
cases (body 1,2,3,4).
The table shows the resistance coefficients c. with respect to t~e
surface -Fr2
B
Card 2/5

On a Class of Bodies of Rotation With
ACA
A 8
A D
3-
0.4
A
0 0.2
Card 3/5
G77Y4
S/040/60/024/005/017/028
C1111C222
a Yinimal Wave Resistance
r

- -A

u
lu
A
' r14-
A
A
\3
A
0 5.4
A 14
14
WA
A
M~_= 4,9
0
A, F4
3
1 M--U

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16L-19

6,11 7 9 4
3/040/60/024/005/017/028
C111/C222
On a Class of Bodies of Rotation With a Minimal Wave Resistance
The author mentiors S.N.Yelisegev and B,M-Kiselov~ He thanks L.N.
Papandina for the programming, There are 3 figures, I table and 4 Soviet
references.
Abstracter's note: (Ref-4) is a paper of the author in Prikladnaya
matematika i mekhanke, 1958, Vol.22, No.2
SUBMITTED: June 16, 1960
Card 5/5

27791
ISZOO S/508/60/02e/000/002/022
D237/D305
WTHORS:
Iordanskiyq S.V.p and Shmyglevskiy, Yu.D. (Moscovi)
TITLE: Sublimation of an axially symmetric blunt body near
the stagnation point of incident gas flow
PERIODICAL: Akademiya nauk SSSR. Otdeleniye tekhnicheskikh nauk.
Inzhenernyy sbornik, v. 28, 1960, 26 - 35
TEXT: The authoxs obtain here the equations of an axially symmetric
laminar boundary layer for a 2-component gas at low temperatures
with diffusion present. Boundary conditions are derived for the
case of sublimation, and the method is given for calculating subli-
mation flow and velocity near the stagnation point. Finally solid
C02 in the stream of air is considered as an example. According to
L.D. Landau and Ye.M. Livshits (Ref. 2: Mekhanika sploshnykh sred
(Mechanics of Continuous Media) Gostekhizdat, M. 1954) the flow of
multi-component gas is described by
Card 1/9
ve

27791
S/508/60/028/000/002/022
Sublimation of an axially ... D237/D305
apw,
-jT,=0.
apc,w, + all- 0,
ax, ax, "alk
PWA: OXk ax, axk
[p (W2 + h)WI - WkCII., +qj] 0,
jX-i 2.
p = p(p, T. cl, c.,...).
(a) (a)
jia pDa (ac a +kT -?T k1) P),
J~7~ +
d x c X p ax
i i 1 (1-3)
qi = [k(a)m TMI 9T
T a a+ Ila J a 7i-iI ve
Card 2/9

27791
S/508/60/028/000/002/022
Sublimation of an axially D237/D305
9W 6 W owl VwP
d i k 2
i + 7, 'xi-3'6 !j (1-3)
ik -'~ __ (_ ik 7x,,) + ~'ik Ox.;
Xk U
For two-component gas (1.1) and (1-3) are transformed into cylin-
drical coordinates by xi = X, X2 = X co .s 19-, X3= r sinI9~and the
equations of axial flow in (x, r)!7plane are derived in an (st n)
orthogonal coordinate system associated with the surface AB of the
body (Fig. 1). The partials are then
0 = 91 Cos 7 0 %sin + COsr a
Yv- 71-F it as - sin y an, ar 91 + n as an
where R = radius of curvature, y angle between tangent to AB and
x-axis at the given point. Tangential and normal velocities u and
v are given by
Wr = u siny + vcosy, wX = ucosy-vxiny.
Then for a small velocity of sublimation
Card 3/9

Sublimation of an axially ...
27701
S/50Y60/028/000/002/022
D237 D305
drpu + ~Mpu . 0,
Ts- (its
pit ac + pvt = ipD & k TOT)'
Ts On On Mn + T On
Pit Lu + P Ou . _dp + ~. au
as Vd-n Ys an 71 Tn
8p = 0 DIV,
D7, HAII P = P (S),
pit a (h + --EI) + pv 2 (h + 2-) = -2- u2 +
FS 2 On 2 On an 2
+ % 2-T + pD (11. - ho + krM) I ac + kr aT
an k7jn_ T WA )11
(1-4)
is obtained, where M = Ma + MP. For low temperature work in the ab-
sence of chemical reactions,
p = mR (--2- + 1 - c)PT, h = ch + (1 - c)h,,
m a M a IJK
Card 4/9

27791
S/508/60/028/000/002/022
Sublimation of an axially ... D237/D305
can be utilized, where c is independent of o and T. Boundary condi-
tions when gas a flows around a body P are for ~ = oo, ,
f oo 1 (2. 1), T N , oo T 0~) - C 00
e
Ce(s), (2.2)
where T and c are the temperature and concentration of a
e e
and for 0
f 0) = 0 (2-3), T(~, 0) = T (p 07)) (2.9)
w e
[(2~fE+f)c-L.L(c.x+LTT,)] =0,
and qT YTE- (2.11)
(2~[E + f) (Q - ckTM) + -~-' T).
P IX-0- ru,pW)j.
where Q [h8(T W)1+0 -[hP(Tw)1_O = heat of sublimation of unit
mass of at the temperature T w a Flow near the axis of symmetry is
Card 5/9

2??91
of an axia7l...
S/508/60/028/000/002/022
D237/D305
solved where -7 the solution can be expressed in the form of a power
series in V.,-, with coefficients dependent on 2,, if p e(,e-) can also
be expanded in powers of 1/,-7. Terms independent of will then giv
a solution on the axis of symmetry. In dimensionless magnitudes
T
t = - mR
T.JE-O MRTWIE-0
Ll
(D~Ifu, F=f), K= CA + TA)
T
E ix + K (H + kl-kO.
P
(D i
(DX = -f T-72 _F2
Fx ~ CD ,fx = F,
T
Card 6/9

27791
S/508/60/028/000/002/022
Sublimation of an axially ... D237/D305
tx=
71 MAC 0) (3-1)
p" Ir tX, I(X fcx,
cx - EF - T
E), - - f (Hcx + Ttx).
is obtained and the boundary conditions (2.1)-(2-3)p (2.9) and (2.
11) become F(O) = 0, t(o) = 1, K(O) = -f(0)0(0),
E(O) = - f(O)[i~ + H(O)c(0)1, (3.2)
F (co 1, too= !e , c (00
. T w
m Q mRT2 dp
(X - -w e
where mRT Pe dTW
Card 7/9

27791
S/508/60/028/000/002/022
Sublimation of an axially ... D237/D305
For flow without diffusion (3-1) can be used if its 5th and 6th
equations are replaced by
K(~.,) z Ot c _ (0 when f < 01
1 when f > 01
and for the flow without sublimation (3-1) can be used with the
boundary conditions
F(O) Ot t(o) it f(0) = 0' C(O) = 1,
F(co 1, t(oo = Te/TW? c(oo ) = 1,
where Tw = given temperature. The problem of the flow of air M
6.2 around the body composed of soli4 C02 is solved as an example,
'There are 3 figures and 11 referencest 3 Soviet-bloc and 8 non-
Soviet-bloc. The 4 most recent references to the English-language
publications read as follows: J*A. Fayp R.F. Riddelp Theory of
Stagnation Point Heat Transfer in Dissociated Air, J#_Aeron. Scl
vol. 25, No. 2p 1958; Tables of Thermal Properties of Gasesp US.
Department of Commerce National Bureau of Standards, Circular 5'..
Card 8/9

27791
S/50 60/028/000/002/022
Sublimation of an axially D237%305
1956; R. Bromberg, R. Lipkis, Heat Transfer in Boundary Layers
with Chemical Reactions due to Mass Addition, Jet Propulsion, vol.
28, no. 10, 1958.
SUBMITTED: May 25P 1959
Fig. 1.
vir
Card 9/9

Computation Practice of Horizontal (cont.) SOV/5608
Center of the Academy of Sciences USSR) has been deriving
experience from the use of this method since 1955. The authors
thank P. I. Chushkin. There are 11 references: 8 Soviet.,
1 English, 1 Frenchyand 1 German.
TABLE OF CONTENTS:
Introduction 3
Ch. I. Method of Characteristics 5
1. Equations and their characteristics 5
2. Elementary problems 9
Problem a 10
Problem b 14
Problem c 17
Problem d 19
Problem e 20
3. Remarks on established formulas and methods 23
4. Numerical examples of solving elementary problems 25
Card 2/3

CHSHKII., I P.I.; SHULISIJIIIIIA, N.P.; ShY.YGLEVSKIY, Yu.P., otv. red.;
ORLOVA, I.A., red.; POPOVA,- . .. tekhn. red.
[Tables for supersonic flow around blunt-nosed cones] Tab-
litsy sverkhzvukovogo techeniia, okolo zatuplennykh konusov.
Yaoskva, Vychislitellnyi tsentr All SSSR, 1961. 91 P.
(MIRA 15:1)
(Aerod3mar.ics, Supersonic-Tables, etc.)

S/0,1z 61/016/002/005/005
C llt~ C 222
U J, F11-3 I I J . A. , Xoiueyev It. N.
Chuahkin P. Z, and Sh=-jrgloT-
3i--y Yu. D,
71-,L-IS Avatol4y Alekseycvich- DorodnItsyn (on the occauion of
his 50", birthday
PERIODICALi UipekhL ca-ematicheakikh nauk, Y, 16, no. -2, 1961,

T::T T ,A. A. Dorodni t-3y-n wi-9 born on De~:eaber 2, 1910 in the dialtrict
T'.11a, 1:1 193! he ftnighed the study at the Mming Fucullty of the
F~.--roleum Ins-.itute Grcz-i:jy.. 3~.nc- 1955 he worked-in the Glaynaya
geofizlc~cokaya obnarraoriya (Geophys,_ca! main Observatory) in
LunlnFrad under the leadirg of J. A.. K,-bell (school of IT. Ye. Kochin).
!a 1939 -- candidate of physical-mathematical sciences.- Sinc.0 -1941 he
va!3 'n the Tsentral*nyy aer,,Kidrod_,namichq1C.Y in3titut imoul N. ie..
Zhukov3kogo ~Central Aerohydrodyramix Institute imeni N. Ye.
2;hukov:;1-_,y). In 1942 -- Doctor dissertation "Boundary layer in a com-
pressible gas". In !955 -- zGmbor of the Academy of Seteacewof the
Card V-1

3104216-;1016100210051005
Anatol :.y A, PR,33yo-.-,i c1l DTr~rln--, t,,yn C i C 2 22
JSSR, '9~~
77ch4s'-telInyy tsentr
nrv-~;k SSSi tne Acade=y-of S!I~-encen USSR).
-,5ent ut the Chalr of Higher
46 - llrcfes~or
in thc- ln3tl*ute; 11944-'1;
a- tiie Ch-i-r o~ Th,r-re-iral, ,-jrodynamcs of the Mo3kovskly av-.Ptalloanyy
S, 0:-dzhon-k.,dz- (M-,31-ow AV-,LLtioa Inutitutu i=:ni S.
Z,~rxce ',9-'7* - P:'ofessor and 1~,ader of* the Chair of Gas
Dynarj-c~ of the I'Loskove3k-.v f,.z-,ko-tokhnicheskly institut (Moscolf
Phyr,;.cal -Technical Inq~:tu-,,j).. Furthermore - President of the Ko:zissiya
p0 'rfrhir-;tjl~noy tokhnke A-q SSSR (Committee of Compu-t-ing', Technics
of th-3 Academy of Bcicacea USSR)l mezter of the Komitat p0 Leninskim
premiyan ~committee for Lenin PrIzes)l preS4 dent of'tha eks-pertnay&
k-.3s::ya VAK po av-omalizra"ii i priborostroyzziya (Comm:it-tue of -
of the VAX 'or Automazizat,-oz and Construction o-f-Equip-ment)
Cli-Jef edlitor of tne "Zhurnal TYchislitellnoy matezatiki I ratematiches-
koy fi--iki (;-irnal a' -.~",)uting mathematics and --athematical physics).
A. A. DorctLn-tqyn p;L-,t-c3pa*ed in the follow;ng congresiest Sweden
in 1957i USA in i958; France in 1959; Poland in 1959; SPaln in 19581
Card 213