SCIENTIFIC ABSTRACT GRIGOROV, N.L. - GRIGOROVA, L.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000516720018-1
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: July 27, 2000
• Sequence Number: 18
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

GINZBURG, -,I. I.
Remarks on the upper zone of weathering qurfa,-e. Kora vyvetr.
no.5:374-379 163, (MIRA 16:7)
1. Institut geologii rudnykh mestcrozhdi~niy, petroggrafil,
mineralogii i geokhimii AN SSSR.
(Weathering)

I.I.; ANDRUSHCUNK0, P.F.
GJNZBURG, ,
- ---7- - " "'..S.o,me results Of the conference on the Componition Of
metallogenic and forecasting Maps Of SuPergene nic"91
deposits. Kora vyv,tr. no.6:312-318 163. (MIRA 17:9)
1. Institut geologil. rudnykh mer3toro;,il*n Yj petrografii,
mineralogii i geokhimii AH S5SR, Mcs~,ia.

GINZBURG, I.I.
Fragments of reminscences. Och.po ist.geol.znan. no.lls46-49 163.
(KIRA 16%7)
(Vernadakit, Vladimir Ivanovichp 1863-1945)

GIW,BURGY 1. 1.
KArBt and ore formation. Trudy MOLP 12x46-53 164. (MIRA 1881)

GINZBURG, I.M., inzh.
Automatic control of the load on a scraper motor. Mekh. stroi.
16 no.]-1:17-18 N 161. (IMIA 16:7)
(scrapers) (Automatic control)

USSR/Physical Chemistry Molecule, Chemical Bond. B-4
Abs Jour : Referat Zhur - Khimiya, No 1, 1957, 141
Author : Ye.F. Gross, I.M. Ginzbur[..
Inst
Title Spectra of Composite Scattering of Crystal of K)let--ular
Compounds.
Orig Pub Optika i spektroskopiya, 1956, 1, No 5, 710-714
Abstract With a view to investigate the influence of the formation
of molecular comDounds on spectra, the spectra of monocrys-
tals SbCl (I) and SbBr3 (II) were studied. Low frequen-
cies of On cm-1) 35, 50, 66, 96 and 63 and frequencies of
intra lecuiek oscillations QMO) of 133, 152, 317, 342
for I and 92, 110, 227 and 236 for Il were fo d. The mi-
nimpm and maxlTmim moments of inertia (IX . 10 and IY -
10-40 g x sq.cm) of the molecules of I and II are:
Ix = 303 and 696, Iy ~~ 523 and 1210. The low frequencies
are satisfying the relation 2 2
Card 1/3 1 / 2 = 12/ Il (1) valid
USSR/Physical Chemistry - Molecule, Chemical Bond. B-4
Abs Jour Ref Zhur - Khimiya,, No 1, 1958, 141
for the frequencies of the rotational oscillations in iso-
morphous crystals. The low and the IMO frequencies of
2SbCl3* CA (III) and 2SbBr3-C6H6 (iv) are as follows:
22, 43, 64, 83, 110, 117 (111); 22, 42, 58, 71 (IV);
and 136, A2, 312, 327, 350, 606, 989, 1176, 1573, 1607,
3062 (111); 89, 102, 213, 225, 241, 990, 3o65 (IV)-
The comparison of the spectra of I, II, III and IV leads
to the conclusion that the low frequency spectra of I, II
and III, IV differ essentially, while the DIO frequencies
of III, IV coincide with the IMO frequencies of 1) 11 and
C6H6' Consequently, the molecules of I, II and C6H6 move
in lattices as a whole with reference of one -to another.
The frequencies 22 and 112 - 43 of III and IV refer to the
rotational oscillations of C H6 - The frequencies 64, 83,
1-10 (111) and 42, 58, 70 (I~j satisfy (1) and correspond
to the rotational oscillations of the molecules of I and
Card 2/3
OWN
I

YAL'TO)OVI A.V.; GINNORG, I.M.
Derivativos of Imidazole. Part 34. Zhur. ob. khim. 34 no.51
1624-1633 My 164. (KIRA 1717)

RPL
-L201--66 'EWr.(m)1'EPF(C)/EW[2q~1EV1A
7CCESSION NR:' ARS014392 UR/0058/65/000/004/DO29/DO29
SOURCE: "Ref. zh. Fizika, 0220
AUTHOR: Ginzburg, 1. Mywy
TITLE: Investigation of the Mdrogen bond?in trifluoroacetic acid-eater systems
by studying their-infrared spectra
CITED SOURCE@ Sb.'Spektroakopiya. M., Nauka, 1964, 167
TOPIC TAGS: IR spectrum, fluorinated organic compound, acetic acid, ester, spec-
trographic. analysis, chemical bonding
TRANSLATION: The IR spectra of trifluoroacetic acid-eater systems are studied.
Spectra for mixtures of these materials always show a band for undisturbed C=O os-i
cillation in the ester, and no bands which correspond to acid dimers. This shows
that the esters form a hydrogen bond with oxygen atoms in the carbonyl and alkoxy
radicals. When there is an excess of acid, a 1785 cm-1 band which corresponds to
acid dimers appears in the spectrum side by side with bands for free and bound
carbonyl radicals in the ester and the acid carbonyl band. It is concluded that
the molecules in the eater form a strong hydrogen bond only with one molecule of the
the-:expense of some single oxygen molecule. Yu. Kissin.
L+_2~1 4Z_1_ RUB-CODE:--OC,-OP-----.---- ENCL:_.OO__:___

Use -T

G-INBURG'. 1.14.~ PETWY, E.S., SITATOITSHTER1, A.I.
~~-Compar.leon of the aleuf.ron-dunor properl,les of the series
of allphal.le~ and cy,.,I--*!:: t3tht,:~a during Interaction wi-bh CH30D.
, Zaur. ob. kh:Ri. 34 no,",'.12;~94-2298 Tl "' ' (MIRA 1! a8)
--- 04

GINZBURG., I.M.; LOGINOVA, L.A.
Spectroscopic manifestations and energy of the intramolecular
hydrogen bonding in thiosalicylic acid. Dokl. AN SSSR 156 no.
6:1382-1385 Je 164. (MIRA 17:8)
1. Leningradskiy khimiko-fe-rmatsevticlieskly Institut. Predstavleno
akademikom A.N. Tereniym.

GINZBURGY I. P.
"on the Question'of the'Motion of Real Gases at High Velocities,"
Ucheniye Zapiski LOU, No.42, pp. 5-60, 1939 . --I
Dissertation for the degree of Oachelor of Physico-Mathematical Sciences.
Presented in December 1937.

f re-
s
L P
b
O
th
th
o
t
6i ~ia
.
s
ur
e
a e
ye
n
e
.;rTs
ry o
. tion. Using certain. transformations the author obtains the
6
'
tate n V. S
U i Annal
eningra [Uclic ye ISM] formula of Kochin. Tim resistance force i's determined
The
rNlaffi. Ser. 13.. Nfechanics~, 135-144 (1944). (Russian) .
author shows that in the case when the i a
rumersed lxxly is
16482]
I
"~
f
h~j
h
h
i
sphere Kochin's formulae agree YAth those of Michell.
o
e
ng the met
t
~n the present paper the aut
or, us
S. Btrgman Cambridge
Mass
).
I;Orier integral, gives a new terivation of a formula of
'
f .
-
,
ransactions of the Conference on the Theory o
Kmliin C1
Wave Resistance, Moscow, 1937].- The. potential v is a
Finction which satisfies the equation 0.
and the boundary conditions at z-0 and
ro cog (n, x) along the -boundary, -where h and ~ ore I
F:iven c6natants and ts the interior normal to the surface kit I '
0w body. Tile author assumes the solution forP 14 tile forip
j
in f f" yjI_ zI)d "d9f,jexPr-k(z+fJ+iI
SE
2
r
4
+ F(k, 0) ex Cks+ k-]Idk
P
where F(k, 0) is ar. explicitly -given junction, B is the
holuidary of the body,_ds is a surface clement of
t
iu~(x-xj) coq0+(y-yj)rin0and (r(Xj,Yj,ffj) 6 a functioll
Whit li -riM. k- determikA by solving a Whear integral cqua.

Sourcet Nathematical Rerlews, Vo No.117

'W~
I 'AWN,
E
0-H Iffififfl,
M.
jmig

T3TTTr
1 . T~Is , _,. 1. P., BOPETSKATA, B. A., OZTI-,r-,OV..'.. A. I., L'IFOG-VA, A. N.
2. ussR (6oo)
4& Manganese Ores - Polunochnoye Deposits
7. Study of the composition of the manganese ores of the Polurochncye deposit.
(Abstract.) Izv. Glav. upr. geol. fon. no. 2. 1941(.
9. Montt-ly List of Russian Accessions, Library of Congress, March 1953. Unclassified.

GINZBURG, I.P.
Sufficient
yftpy$,tq.r
stability conditions for the solution of
= 0. Uchsap.Lon.un.no.114:200-204 149.
(Squations, Theory of)
the equation;
(MLRA 10:3)

GINZBURG, I-P-
Xquations for
no.114:205-216
the motion of v&riable-mass solids* UchesapeLaaouno
149. (KLRA 10:3)
(Notion)

TJSSR/Physics Hydraulic, Impact Jun 52
"Computation of Hydraulic Impact in Pipes With
Variable Cross, Section," D. M. Volkov, I. P. Gins-
burg
Vest Leningrad U, Ser Mat, Fiz, Rhim, Vol 7, No 6,
yp _~,9_46
Generalizes results by I. F. Livurdov (Iz ArtilUr
Mad imeni Dzerzhinskogo, 1.8 (1944)) for the cum
vhere wall thickness of pipe and sound velocity are
variables., an& presents solutions of problem for a
wide IcIass of pipes vith variable cross sections.
251T100

G
On sufficient stability conditions of zero solutions for n-order linear
homogeneous differential equations and n-homogeneous differential
equation systems with variable coefficients. Vest.Len.un.9 no-5:53-65
NY 154. (Differential equations) (MI-RA 9:7)

GINZBURG, I-P-; GRIB, A-A-
v------- IM"010-
Water hammer in a complex condLuits. vesz.bensuno
Vest.Len.un. 9 n0.8:107-128 Ag 154.
(Water hammer)
no.8:107-128 Ag 054.
(MLRA 8:7)

USSR/hysice 6~8' flow
Card 1/1 Pub. i27 6/12
Authors I Gineburg, I. PO
Title I Stabilized outflow of a gas from the containers producing friction and
local resistances
Periodical t Vest. Len. un. ser. mat. fiz. khim. 5~ 55-84, May 1955
Abstract I A method of computing the amount of gas flow from a container, considering
friction and local resistances, is described. Various cases of gas flow
(adiabatic, long pipes with thermal or isothermal processes during the
flow) are considered. Tables; graphs; diagrams.
Institution
Submitted April 16, 1954

(j, T, V,
12-1-11-11679
Translation from: Referativnyy Zhurnal, Mekhanika, 1957, Nr 11, p 51 (USSR)
AUTHOR: Ginzburg, I. P.
TITLE: The "Water Hammer" in Pipes Made of Elastic-Viscous Materials.
(Gidravliclieskiyudar v trubakh iz uprugo-vy-azkogo materiala).
PER1061CAL: Vestn. Leningr. un-ta. 1956, Ni 13, 99-.u8
ABSTRACT- The A. establishes the equations of the water hammer in a thin-walled
pipe having a varying diameter along its length and consisting of an
elastic-viscous or plastic material. Discarding the convective terms
and assuming a linear frictional function, these equations are reduced
to a single differential equation of the fourth or third order. A general
solution for this equation is offered for the case of a cylindrical pipe,
obtained by means of a Laplace transformation.
Bibliography: 5 references N. A. Kartvelishvili
Card 1/1

AKSMOV, I.P.; GINZBURG _I P... prof., doktor fiziko-matemat.nauk, nauchnyy
rukovod-Ail 1--- 1- IR A--.
(Determining the surface temperature and surface friction of cones
and a certain class of axisymmetrical bodies of revolution moving
with high supersonic speeds; dissertation presented for the douse
of dandidate of Physicomathematical Sciences] Opredelenis tempers-
tury na poverkhnosti i poverkhnoatnogo treniia konueov i nekotorogo
klassa osesimmetrichnykh tel vrashchaniia, dvizhushchikheia a
bol'shimi averkhzvukovvmi skorostiami; avtoreferat dissertateii
na soiskania uchenoi stepani kandidato fiziko-matematichaskikh
nauk. Leningrad, 1957. 7 P. (MIRA 12:8)
(Aerodynamics, Supersonic) (Friction)

SOV/124-58-8-8424
Translation from- Referativnyy zhurnal, Mekhanika, 1958, Nr 8, p 12 (USSR.)
AUTHOR: Ginzburg, _I- P.___
TIT LE: Basic Equations for the Dynamics of the Control of Water Turbines
(0snovnyye uravneniya dinarniki regulirovaniya gidroturbin)
PERIODICAL: Uch. zap. LGU, 1957, Nr 217, pp 144-184
ABSTRACT: The article gives a detailed account of the derivation of an
equation for the process of controlling a water turbine with the aid
of a hydraulic regulator. Equations are given for the turbine con-
trolled, the sensor element, the servomotors, the gate valve, and
the penstocks. The equations evolved are compared with those
appearing in the fundamental work on turbine control by A. Stodola.
The present equations, however, are not investigated.
M. A. Ayzerman
Card 1/1

10(0) PHASE I BOOK EXPLOITATION SOV/2053
Ginzburg, Isaak Pavlovich
Prikladnayn gidrogazodinamika (Applied Hydro- and Gas Dynamics) /Leningrad/
Izd-vo Leningr. univ., 1958. 337 P- Errata slip inserted. 4,000 copies
printed.
Sponsoring Agency; Leningrad. Universitet imeni A. A. Zhdanova. Redak-
tsionnoizdatellskiy movet.
Ed.: Ye. V. Shchmeleva; Tech. Ed.: S. D. Vodolagina.
PURPOSE: This teytbook is for students of physics-mathematics and mathe-
matics and mechanics departments at universities and other institutions
of higher learning. It may also be Useful to engineers and scientific
personnel conerned with problems of design and research on engines, gas
exhaust, pneumatic installations, etc.
Card 1/11

Applied Hydro- and Gas Dynamics SOV/2053
COVERAGE: This textbook on applied hydro- and gas dynamics is based on a
series of lectures on mathematical mechanics given by the author at the
Leningrad State University. The book develops the basic equations of hy-
draulics and the theory of similitude emd dimensional analysis. It treats
uniform and unsteady motions of fluids and gases in straight and cur7ed
pipes of uniform and varying cross section, the discharge of fluids and
gases from containers, the time required to fill and empty vessels, and
the reactions of flowing liquids and gases on rigid boundaries due to mo-
mentum changes. Examples of the application of these methods to part-
icular engineering problems are presented. Problems of airfoil and cas-
cade theory are not discussed since they are ful-ly treated in other books,
such as Prof,:~ssor G. N. Abramovich's Prikladnaya Gazodi'aamika (Applied
Gas Dymmics).; etc. In view of Professor K. P. Stanyakovich's detailed
monograph Neustaaovivsheyesya dvizheniye sploshnoy sredy (Unsteady Notion
of a Continuous Medium), the unsteady motion of gases is considered only
in connection with the emptying of vesiaels. Similarly, problems of un-
steady motion of a fluid in rivers and channels are not considered since
they can be found in the article by Academician B. A. Khristianov-ich
Card 2/11

Applied Hydro- and Gas Dynamics
SOV/2053
'Unsteady Motion in Channels and Rivers", in the collection Nekotoryye no-
v-yye voprosy mekhaniki sploshnoy sredy (Some New Problems in the Mechanics
of a Continuous Medium) and in V. A. Arkhangelfskiyts monograph Raschety
neustanovivshegoeya dvizheniye v otkrytkh vodotokakh (Calculation of an
Unsteady Motion in Open Water Currents). There are 69 references, 65 of which
are Soviet, and 4 translations from German.
TABU OF CORrMS:
Preface
3
Ch. I. Basic Equation of Hydraulics
1. Hydrodynamic quantities and their average values. Basic concepts and
definitions 5
2. System of equations of motion of a fluid 9
3. Internal energy., specific heat, viscosity., and heat conductivity of
fluidsand gases 18
Card 3/11

Applied Hydro- and Gas Dynamics
SOV/2053
4. Equations for mean local hydrodynamic quantities 25
5. Hydraulic formilation of the problems and equations of hydraulics 29
6. System of equations of the hydraulics of an incompressible fluid.
Bernoulli I a equation 42
7. Examples of the application of Bernoulli's equation to an incom-
pressible fluid 44
Bibliography
Ch. II. Basic Theories of Similitude and Dimensional Analysis
1. Determination of similitude 48
2. Basic lave of mechanical similitude 49
3. On approximate similitude 54
4. Relationship betveen similitude and di nsions. V- theorem 55
5. Examples for application of the IT theorem 6o
Bibliography 64
Ch. III. Uniform Motion of a Fluid Through Pipes and Channels
Card 4/11
Im
ANT
W,

Applied Hydro- and Gas Dynamics
SOV/2053
1. General relationships for the uniform motion of a fluid in a
pipe 65
2. Laminar motion of fluid in a circular pipe 67
3. Limits of applicability of the laws of laminar motion of a
fluid. Phenomena, occurring in the initial section 69
4. Transition from laminar to turbulent flow. Critical Reynolds
number. Phenomenon of intermittent turbulence 71
5. Results of the experimental investigation of the turbulent
motion of fluid in smooth pipes 73
6. Relationship between the friction law and the law of velocity
distribution across the cross section of a pipe 77
7. Basic aspects of the semiempirical theory of turbulence up-
plied to the motion of a fluid through a pipe 81
Turbulent motion of fluid in rougb pipes 89
9. On the turbulent motion of a fluid in non-circular pipes 95
_BIW4ography 96
Card 5/ .11

Applied Hydro- and Gas Dynamics SOV/2053
Ch..17. Unsteady Motion of a Fluid in Pipes
1. Equations of motion of a fluid in pipes 97
2. Equation of state. Internal energy and entropy of the fluid 98
3. Equation determining variation in area of a pipe cross
section as a function of pressure 104
4. Boundary and initial conditions 108
5- Solution of the problem of unsteady motion of a fluid in a
pipeline without consideration of compressibility 123
6. The work of N. Ye. Zhukovskiy on hydraulic shock in water
pipes 117
7. Hydraulic shock in pipes of variable cross section 121
8. Problems of regulation in the presence of hydraulic shock 133
Bibliography
ChX'V. Motiom,.of.Wnseg insPIpes
139
1. Equations of motion 140
2. Equations of the steady motion of a gas. Concept of
critical speed 142
3. Motion of a gas in pipes of variable cross section 146
Card 6/1-1

Applied Hydro- and Gas Dynamics
SOV/2053
4. Adiabatic motion of a gas in a pipe of variable cross section.
The I&Tal nozzle 147
5. Motion of a gas in a heat-insulated pipe in the absence of an
internal beat source 152
6. Notion of a gas in a pipe of constant cross nectioa in the pres-
ence. of a heat source 156
7. IsotbArnal action of a 9" in a Pipe 165
8. Isminar notion of a W in flat and circular pipes 166
Bilaiogmjhy 177
Ch. IX.,.,~ Local-ResIstAmpsh,. Motion. of a Fluid and a (Ins in CurvocL PipeaL
1. Motion of a fluid in a pipe with a sudden change in amen
section 178
2. Notion of a gas in a pipe with a sudden change in cross sec-
tion. Shook waves 186
Card 7/11

Applied Hydro- and Gas Dynamics SOV/2053
3- Notion of a fluid in diverging and converging pipes 194
4. Notion of a fluid in nonstraight pipes and channels. Curved
pipes 199
5. Basic conclusions from the results of experimental investiga-
tions for determining the local-drag coefficients for branch-
ed pipe lines, lattices, nets, etc. 205
Bibliography 214
Ch. VII. Stea4y. Disakale of. fluids and GeAes from Veaffels , SVill-a
W".
1. Discharge of fluid from smiall and large openings 215
2. Discharge from nozzles 218
3- Theoretical methods for determining the coefficients of jet
contraction 219
Spillways. Determination of the discb~xge of fluid through
a spillvay. Spillway vith a wide silI 225
Adiabatic discharge of a gas from a vessel through a small
opening. Analogy with a spillway having a wide sill 233
Card 8/11

Applied Hydro- and Gas Dynamics
SOV/2053
6. Dischargecea, gas from a vessel through a long heat-insulated pipe 236
7. Discharge uf a gas from a vessel through a long pipe for the case of an
isothermal process of gas flow in the pipe P-42
8. Discharge of a gas from a vessel through local resistances 245
9. Discharge of a gas from a vessel through a long pipe and local
resistances 254
10. Discharge of a gas from a vessel through a long pipe in the case of
laminar flov conditions 257
Bibliography
Ch. VIII. Determining the Time Required for Filling and Emptying Vessels
263
of Fluid or Gas
1. Determining time required to empty fluid from a vessel under the
assumption of a quasistationary outfl(rr process 264
2. Solution of the problem of determining time required for
Card 9/11

Applied Hydro- and Gas Dynamics SM/2053
equalizing the water levels in two lock chambers 22-66
3. Approximate solution of the problem of emptying a vessel without
the assumption of a quasistationary outflow process 267
4. Solution of the problem of determining the time for emptying a vessel
of gas flowing through local resistances or a long pipe line and assum-
ing the process of outflow to be quasistationary 270
5. Exact solution of the problem of emptying a cylindrical vessel of gas
flowing through a small opening in the bottom. Reflection of a shock
wave fromthe wall' with the opening 274
6. Determining the time for filling a vessel with gas 29k
7. Solution of the problem of emptying a variable-volume vessel of gas
in the presence of internal fuel combustion 296
8. Determining pressure as a function of time in a chamber where the com-
bustion of solid fuel takes place 300
9. Solution of the problem of sinultaneous filling and emptying of a
vessel of gas 305
10. Examples of engineering applications of the above-mentioned problems 309
Card 10/11

Applied Hydro- and Gas Dynamics SOV/2053
Bibliography 32-1
Ch. IX. Lave of Momentum and Moment of Momentum and Their Application to the
Solution of the Problem of Interaction.Betveen a Flav and Rigid
Boundaries
1. PresmLre of liquid and gaseous jets on stationary and moving obstacles.
The Pelton vhedl 322
2. Determination of the forces and moments with vhich the moving fluid
(gas) acts upon the vessels conducting them 329
Bibliography 334
AVAILABU: Library of Congress (QA 911 . G49)
IS/bg
7/14/59
Card U/U

KOVAJAW, Wiksim Antonovich; BELOVA, Alekoandra Vasillyevna; MAROVICH.
Hatallya Mikhaylovna; LANDW, Vera Gennadiyevna; GI.TZBURG,
I.P., prof., red.; BUSORGINA, N.I., red.; ZffUKOVA, Ye.G.,
tekhn.red.
[Manual for laboratory work on aerognadynamics] Rukovodstvo
k laboratornym rabotam po aerogazodinamike. Pod red. I.P.
Ginzburga. Leningrad, Izd-vo Leningr.univ., 1959. 175 P.
(MIRA 13:1)
(Aerohydrodynamics--Hondbooks, manuals, etc.)

PHASE I BOOK aPLOITATI011 50V/5290
Soveshchaniye po prikladnoy gazovoy dinamike. Alma-Ata, 1956
Trudy Soveshchaniya po prikladnoy gazovoy dinamike.. g. Alms.-Ata, 23-26 oktyabrya
1956 g. (Transactions of the Conference on Applied Gas Dynamics, Held in
Alma-A+a; 23-26 October 1956) Alma-Ata, Izd-vo AII Kazakhskoy 53R, 1959.
23) p. Errata slip inserted. 900 copies printed.
Sponsoring Agency: Akademiya nauk Kazakhskoy SSR. Kazakhskiy gosudarstvennyy
universitet imeni S.M. Kirova,
Editorial Board: Resp. Ed.: L.A. Vulis; V.P. Kashkarov; T.P. Leontlyeva and
B.P. Ustimenko. Ed.: V.V. Aleksandriyskiy. Tech. Ed.: Z.P. Rorokina.
PURPOSE- This book is intended for personnel of scientific research institutes
and industrial engineers in the field of applied fluid mechanics, and may
be of interest to students of advanced courses in the field.
Card 1/9

Transactions of the Conference (Cont.) SOV/5290
COVERAGE: The book consists of the transcriptions Of 31 papers read at the
conference on gas dynamics which was convened under the initiative of the
Kazakhskiy gasudarstvennyy universitet imeni S.M. Kirova (Kazakh State Univer-
sity imeni S.M. Kirov) and the InGtitut energetild Akademii nauk. Kazakhskoy
SSR Institute of Power Engineering of the Academy of Sciences Kazakhskaya
SSR) and held October 23-26., 1956. Three branches of applied gas dynamics
were discussed, namely: jet flow of liquids and gases, aerodynamics of furnace
processes, and the outflow of liquids. The practical significance of the
"Transaction0lof the conference consists in the adaptation of theory to
methods of technical computation and measuring methods related to industrial
furnaces and other industrial processes in which aerodynamic phenomena play
a predominant role. Eight papers read at the Conference are not included
in this collection for various reasons. The authors of the missing papers
are: L.D. L'vov (Thermal and Aerodynamic Characteristics of Pulverized Coal
Flame Burners) and A.A. Goleyevskiy (Outlines and Physical Models of the Jet
Motion Mechanics of Fluids), N.I. Akatnov, Ye. P. Bogdanov, S,V. Bukhman,
T.K. Mironenko, A.B. Reznyakov, and G.V. Yakubov. L.G. Loytsyanskiy is
mentioned as being in charge of a department of the Kazakh State University,
and I.D. Malyukov, Candidate of Physical and Mathematical Sciences, Docent,
as a member of the saxw university. "Ieferences are found at the end of
most articles.
Card 2/9

I
Transactions o" the Conference (Cont.) SOV/5290
TABLE OF COInWITS:
From the Editors
Session of October 23, 1956
Abramovich, G.N. (Doctor of Technical Sciencec; Professor; TGIJV4
imeni Baranova 11'entral Scientific Research Institute of Aircraft
Engines imeni P.I. Baranov], Moskovskiy aviatGionnyy institut imeni
Ordzhonikidze, Moskva (Moskow Aviation Institute imeni Ordzhonikidze,
Moscow]. Turbulent Jets in a Flow of Liquid
Ginzburg., I,P. (Doctor of Physical and Mathematical Sciences;
J~iofessor; Gosudarstvennyy universitet imeni Zhdanova., Leningrad
(State University imeni Zhdanov, Leningrad]. On the Outflow of
of Gases From Containers Through Pipes in the Presence of Friction
and Local Resistances 17
Card 3/9

Transactions of the Conference (cont.) SOV/5290
Vulisp L.A. [Doctor of Technical Sciences; Professor;
Kazakhskiy gosudarstvennyy universitet imeni Kirova;
Institut energetiki. AN KazSSR., Alms.-Ata, (Kazakh State
University imeni Kirov; Institute of Power Engineering
Academy of Sciences Kazakh SSR, Alm Ata)]. Basic Results
and Further Problems of Investigating Jet Motion of Liquids
and Gases 29
Isatayev,, S.I. On the Turbulent Wake Behind a Poorly
Streamlined Body 59
Contents of the Discussion In Brief
Session of October 24, 1956 (Morning)
44
Antonova., G.S. Investigating Turbulence Characteristics of a
Free Nonisothermic Jet and an Open Flaw 45
KashRarov., V.P. (Candidate of Physical and Mathematical Sciences].
On Parallel and Contrary Motion of Two Uniform Flows of ComIressible Gas 55
Card Val

Transaction-, of the Conference (Cont.) SOV/5290
Leontlyeva, T.P. (Candidate of Technical Sciences]. _7xpansion of
Axially Symmetrical Jets in Parallel and Contrary Flovis 62
Bukhman, S.V. Regularity of Motion and Combustion of Coal Particles 69
Nazarchuk, M.M., and N.I. Pol'skiy. On the Crisis in the Viscous
Flow of Gas in a Plane Parallel Channel 69
Contents of the Discussion in Brief 75
Session of October 24, 1956 (Evening)
Terekhina,, N.N. Expansion of an Axially Symmetrical Jet of Gas in a
Medium of Different Density 77
Chebyshev, P.V. (Vsesoyuzn,,y elektrotekhnicheskiy institut (All-Union
Electrotechnical Institute)]. Electrothermoanemometers and Their
Use in Investigating Nonisothermic Gas Flows 85
Card 5h
0- M ~___
?:F~ tn~
Transactions of the Conference (cont.) SOV/5290
Trofimenko., A.T. Investigating a Semirestricted Turbulent Jet 1010
Akatnov., N.I. Survey of the Works of the Department of Hydrottero-
dynamics of the Leningrad Polytechnical Institute imeni Kalinin
on the Jet Theory 107
Shepelevo S.F., and S. Tsoy. Plane Jet in a Cross Section of an
Air Conduit 108
Bespalova) V.G. Use of Hydrointegrators Far Solving Jet Prcblem.- 115
Contents of the Discussion in Brief 122
Session of October 25, 1956 (Morning)
Katsnellson, B.D. (Candidate of Technical Sciences; Docent; Teentral-Inyy
kotloturbinnyy institut imeni Polzunovaj Leningrad (Central Turbine and
Boiler Institute im-ni Polzunov, Leningrad)].
Some Problems of the Aerodynamics of Furnace Cyclone Chambers and of the
Combustion of Coal Powder Pulverized Coal 123
Card 619
SOV/52')O

Transactions of the Conference (Cont.) SOV15290
Yerchin, Sh. A. Aerodjnamica of a Turbulent Gan Flarr~ L6p,
Kokarev, N.I. [Candidate of Technical Sciences; Urallakiy
politekhnicheskiy institut imeni Kirova, Sverdlovsk (Ural
Polytechnical Institute imeni Kirov, Sverdlovsk)]. Industrial
Testing of New Gun Heads of Open Hearth Furnaces 178
Bogdanov, Ye. P. On the Thermal Regime of the Gasification Process 186
Contents of the Discussion in Brief
Final Session, October 26, 1956
186
Zhulayev, P. Zb. [Candidate of Technical Sciences; Docent).
Survey of Work on Hydrodynamics Done by the Institut Energetiki
AN KazSSR (Institute of Power Engineering of the Academy of
Sciences Kazakhskaya SSR) 187
Romarienkop S.V. (Deceased). Basic Problems of Flew Thermodynamics
in Real Boundary Conditions 197
Co-rd 8/9

Transactior.-. o^ the Conference (Cont.)
Vulis, L.A. On the Circular Motion of Ft Viscous Gan
Mironenko, T.K. Effect of the Local Diitribution of I'norgy
in a Iligh Velocity Flow of Gas 215
Lifshitsp A,G, Flow of Doiling and 'Hot Water ThrouCh Conical l'ozzlcj3 n15
Radchen1m, G.A., and P,V. Beloborodov, Concentration Fields of
Highly Dispersed Aerosols in Air Conduits 223
Contents of the Discussion in Brief 229
Decisions of the Conference 2"1
AVAILABLE: Library of Congress
Card 9/9
7-29-61

ram I oam Inum-m -4M/4630
VIoyr
S"'y. lt~t. allp
L-.t
A. A. MW ~-.
P-r- U- 1. 1. T..h. U., T.. G.
ZS!k-.
1 T'tr. e 1. to,
-IM, L_tLizt~.) W-4 d'.t4. WO -I.. for
of rl&l~.
=.'Zflkzr: rt. CIL:-.2- or rict-I in tl., r1,11 of
armt-to. f
31
to tb. 56
X-U-r
of V-4 L~ tZ,~
f~ 3. -111.1. 6.3
%~e of of
a- U~.i Prcloloa of --h, Aztioa
p,,-,,, ft-b of ;,bl-
At.~ ~gr Q-.Y D
t- of :~. yttll
-f RAlt# -11Z4 113
ctb tz tio C- . pio L
of ut-Lb
or
lz the
cc S.-I to tb~ C~se
.M..-d 3tm:4 136
L,--I!ag '_-A,or C-d-n-loo. of . M--1 a.
1h. Y.M. Of tto ll~tlla Cz=G-~ts of Pkir IX7
15. Cbl--, Zr.. -1 X.I. M!t--Tu__. 0~ -b, of
Petzfn-~ ~._ t=Ar-jC'A 156
R"_TICAvMDV(A)=3
16. 'r
166
17. I.P. -d A-&.- 0-1e' '~~ebul-t D.-A~7
170
28 3.'--A,,y Z~por of
136
19. .0 wttm of ~ zu.1 G" L. . T... Of
C_.' Bet._~% 197
2-3. IffT!t T, 'I- D-'h of
M". of .
,.S. Iffact or t.. fepth of m th* Q._tlt7 of t".
As.mi.-.d Mwx of m lallp"id of

GINZBURG, I.P.
(Possible methods for solving boundary layer problems in the
case of dissociation and diffusion; Conference on Heat and I-lass
Transfer, Minsk,, June 5-10, 19611 0 vomrozh-nykh metodakh reshe-
niia zadach pogranichnogo sloia pri nalichii dissotsiatsii i dif-
fuzii; soveshchanie PO t6plO-i Ma6soobmenu, g. Minsk, 5-10 Uunia
1961 g. Minsk.. 1961. 35 P. (MIRA 15: 2)
(Boundary layer) (Dissociation) (Diffusion)

GINSBURG, 1. P.
"On Possible Solution Methods of Problems of a
Boundary Layer at Dissociation and Diffusion."
Report submitted for the Conference on Heat and Mass Transfer,
Minsk, BSSR, June 1961.

GIN-TRI-M..I..P..).OALANOVA).S..S..j.and D24EM2,V, V. G.
"Solution of Laminar Boundary Layer Problems With Regard of
Radiation and Absorption of a MediiAm."
Report submitted for the Conference on Heat and Mass Transfer,
Minsk, BSSR, june 1961.

20762
S10431611000100110041010
OA11 00 C111/C222
AWHORS Ginzburg-, T.P.
TITLEs Turbuleni boundary layer in a compressible fluid (gas
mixture)
PERIODICAL: Leningrad. Universitet. Vestuik. Seriya matematiki, makhaniki
i astralwaii, no.1t 1961, 75-88
TEXTs Starting from the semiempirical theory of turbulence the authqr
gives an approximate solution of the problem of the determination of
skin friction and heat of a plate being in a compressible fluid during
a turbulent motion. Dissociation and diffusion are bonsidered, the
Prandtl number may be an arbitrary constant.
At first the author establishes the stationary boundary lmyor equations
under consideration of the diffusion and the forces due to inertia. For
the determination of the components of the friction tensor and the
diffusion and heat vectors the author uses the results of the semi-
empirical theory of turbulence, where the mixing ways in all cases are
equated. It Is assumed that there exists a laminar lower stratum, where
at the boundary of it the derivatives of the velocity, of the beat
content and the concentration have jumps, while the velocity-, the heat
content and the concentration themselves, as well as the skin friction,
Card 1/3

20762 14.
S/043/61/ooo/oo1/oo4/o1o
Turbulent boundary layer... C111/C222
the diffusion and the heat flow remain continuous. A number of further
simplifications is madet e.g. it is put
T = a h3+b h 2+a h+d, (3-3)
'2 1 11 1 14
where T -- Umperature, Mi -- molecular weight of the i-th
Component, relative mass concentration, h h hi
specific entalpy of the i-th component; the gas is assumed to be
thermodynamically ideal; the friction stress is arranged as a quadratic
polynomial in where y -- coordinatelto the plate, E-- thickness of
the boundary layer. The equations can be integrated under these and
further assumptions. For the velocity distribution in the laminar lower
stratum the author obtains
v I+n V +n v2 (8-3)
x ~ x -~ x 1A j ,
where'C is the friction stress at the wall, whileM. and n are
Card 2/1

20762
S/043J61/000/001/004/010
Turbulent boundary layer... C111/C222
connected by the arrangement
h+dl )n (7-3)
hw+d,
where coefficient of the physical tenacity, h -- the h-value at the
wall. The author determinest 1. The dependence ofwthe full heat content
of the velocity. 2. Velocity profile- 3, Thickness of the laminar lower
stratum and the velocity at its boundary- 4. The connection between ~
and S -thickness of the boundary layer- 5. Law of friction. 6.tomperature
of the surface of the plate- 7- The appearing constants.
The author mentions L.Ye.Kalikhman. There are 2 figures, I Soviet-bloc
and 2 aon-So-iiet-bloc references. The reference to the English-language
publication reads as followes M.Leghthill. J. fluid mech., 2, no.1,1957.
Card 3/3

23154
S/024/61/000/003/002/012
14) 8-3 E140/E463
003/
AUTHORS: Babushkin, S ~). and Ginzbur8-,__I_,~P. (Ler.:Lngrad)
TITLE: On the theory of nonlinear combined and autonomous
control systems
PERIODICAL: Izvestiya Akademii nauk SSSR, Otdeleniye tekhaicheskikh
nauk, Energetika i avtomatika, 1961, No-3, pp.14-30
TEXT; The article attempts to determine the nature of a computer
(analogue) for an automatic control system in which k controllers
regulate that many system coordinates, such that absolute
invariance of the regulated parameters and their autonomy with
respect to the other coordinates of the system be obtained. The
system considered in all generality in shown in Fig.1, where
A, is the object, B the computer, the small blocks labelled
1, ..., V , k are the regulators. Further yj ( V = 1, ..., k)
are the coordinates of the object in k-space, x_i,)(V)
(JV - 1 ... nv) describe the motion of the re-g-ulators,
W (I 'C
xn10 v ... I k) is the action applied by the NP-th
regulator to the object, g.2(t) in the input programme to the
computer, QV = y,# - go(t) are error signals (physically
Card 1/7

23154
S/024/61/000/003/002/012
On the theory of nonlinear ... E140/E463
measured) Etv M (t ) (t.1 . p,4 i V . 1, ..., k) are
exJ nal perturbations acting on object and regul tors, and
X1 ~6 are the computed control signals. Finally, I I are the
functions generated by the computer. Such a system is described
by a system of differential equations consisting of three groups
of equations: equations describing the motion of the controlled
object and the controllers, equations describing the motion of
the computer, and k equations describing the errors. It is
assumed that the equations of the object are fixed while the
equations of the regulators are only slightly varying. The
physical measurements and their conversion to computer input
signals are assumed inertialess. The object and regulator
functions and their partial derivative an well as the computer
functions and partial derivative are assumed continuous and bounded
over the entire range of possible variation. The computer has
k equations for solving the k input signals to the regulators.
In these equations there are initially undetermined equations
describing as yet unknown corrective networks. The problem posed
by the paper can now be stated more precisely. It is required to
determine the conditions placed on the computer functions 4-0,
Card 2/7

S/024/61/000/003/002/012
On the theory of nonlinear ... E140/E463
such that
Y') = 9 V W N = 1, 2, .... k) (1.2)
i.e. that the motion of the object identically correspond to the
input programme, as well as the conditions on the equations of
the individual regulators and the overall automatic control system,
in order that the motion defined by this solution be stable.
Such motion is termed: programme motion. Eq.(1.2) permits the
system of differential equations of the general system to be
simplified by elimination of the static error equations. The
second section of the article is concerned with the derivation of
the simplified equations. This simplification depends on the
fact that for an approximately invariant system, the error terms
in the object and regulator equations are negligible (which is not
true for the computer equations which depend precisely on the
error values). Then a subset of the equations simplify to an
autonomous system of N differential equations in N variables,
which can therefore be integrated'independently of the remaining
k equations of the system. The problem of determining the
Card 3/7
U, Vt9"ffl
im

23154
S/024/61/000/003/002/012
On the theory of nonlinear z14O/E463
computer function is solved by first substituting the functions of
time found for the simplified object and regulator equations in the
general expression for the as yet unknown computer functions.
By the formulation itself of the problem, the steady state values
of the errors are arbitrarily small. Then the functions CO
can be expanded close to the plane in which the errors and their
derivative vanish in a Taylor series in variations of the error
from this plane. This implies that absolute invariance of the
system will occur only when the functions I)v vanish identically
and the partial derivatives with respect to the errors aVe bounded
with substitution in them of the functions of time - kv)
xJ10
where the bar indicates the solution of the simplified system.
Examining further the conditions placed on the functions 41-4,
it is found that one sufficient solution to the problem is
equivalent to a control system using perturbation only. No system
operating on deviation alone can satisfy the criteria of absolute
invariance and autonomy. The author then derives a system of
variational equations which constitute the basis for the final
stage of the solution. In the final section, the author examines
the question of stability of the motion defined by the solution
Card 4/7

S/024/61/000/003/002/012
On the theory of nonlinear ... E140/E463
obtained. The stability problem reduces to the study of the
stability of the zero solution of an homogeneous system of linear
differential equations with variable coefficients. In a
particular case the coefficients of the equations become constants.
It is this particular case which is examined in detail in the
article. The examination is carried out in two stages, firstly
for each of the k coordinates independently and then the system
as a whole. The stability conditions are expressed in terms of
the roots of algebraic equations. It is found that the stability
depends not only on the form of control function, but on the
parameters of the controlled object and the regulators. Thus
conditions can be obtained for the physical realizability of the
system. A brief remark on the general case (where the stability
coefficients are variable) indicates that the dependence on the
system parameters holds here as well. In conclusion the author
mentions various related questions which have not been treated
in the article. The possibility of substantially simplifying the
form of the differential equations defining the regulation function
or even of excluding from these equations a part of the information
Card 5/7

23154
S/024/61/000/003/002/012
On the theory of nonlinear ... E140/E463
external to the the 9-th coordinate system; the elimination of
mutual couplings between the regulators; the possibility of using
self-adjusting corrective networks in the computer and the
inclusion of nonlinear equations in the latter. There are
3 figures and 16 references: 12 Soviet-bloc and 4 non-Soviet-bloc.
The four references to English language publications read as
follows: Moore., I.R. Proc.IRE, 1951, v.39, Noll, pp.1421-1432;
Baksenbom, A.S., Hood, R., NACA, Rep.980, 1950;
Aseltine, I.A., Manicini, A.R., Sarture, C.W., Trans. IRE on
Automatic Control, PGAC-6, 1958; Margolis, M., Leondes, C.T.,
IRE Weson Convention Record, 1959, pt.4, P.104.
SUBMITTED: January 23, 1961
Card 6/7

99G
SYJ45/61/000/004/005/008
10 Q-,IDD D274/D502
AUTHORS: Ginzburg, I.P., and Kocheryzhenkov, G.V.
TITLE: Turbulent boundary layer of heat-insulated airfoil or
axiBymmetric body
PERIODICAL: Leningrad. Universitet. Vestnik. Seriya matematiki,
mekhaniki i astronomiit no. 4, 1961, 115 - 121
TEXT: The problem of gas flow in a turbulent boundary layer is
solved by assuming Pr = 1. Velocity profile: It is assumed that the
friction stress in the boundary layer can be expressed by
_ (Y)2j+ w[(j)_(;L)2]j,
where TW is the shear stress at the wall, the thickness of the
boundary layer and y the distance from the viall;
W 6 dp.
w dx'
Card 1/8

2902'1
-S/043/61/'000/004/005/UO8
Turbulent boundary layer of ... D274/D302
the gas is ideal; equation
T
c h + d (1-3)
holds. Hence
c if + d Hw+ cd
1 w 1 (1-5)
Pw - c1 h + 7 ~ v27
H + d - A x
w c1 2
where Hw is the heat content of unit mass outside the boundary lay-
er. The.equations of semi-empirical turbulence theory are used (in
conjunction with Dlqs. (1.1) and (1-5)) for obtaining the equation
for the velocity profile in the turbulent boundary layer, viz.
--- --- -----
Y +
+ Y (I d
2
PW k2yz
H. + d -A V~
C, 2
Card 2/ a

Turbulent boundary layer of
29027
S/'04y6l/UOU/UO4/005/UO8
D274 D302
The presence of a laminar sublayer is aunumed. There one can appro-
ximately net:
ITw 1 iR Y2 (1-7)
X ~" F,,- y ' Tw d x 2
The velocity at the boundary of the laminar sublayer is
Ti kl Vw 1 + 4 -Tw
u + lk ~i = 1, L (1 ~ L) =
dx 2 2 k v
-V + W 11w
w (19)
ki
;Z~~ -7 V* where v
k -Plww
The derivation is examined of relationship between TW and By
expansion in series (of arc sin kl/k U/g) one obtains from
-'kl k, u 1
7=- [arcsin arcsin -In
k 2 -UC
Card 3/8

SX 29027
u4 bl/000/04/05/00d
Turbulent boundary layer of ... D274YD302
equation
ke,
U6 k 1 e U-arcein u , where D e1-k 1- (2.1)
VV, k -Vi + We 2
In order to find the friction resistance of an airfoil, a second
equation between 6 and T is required. This can be obtained from
w
the law of conservation of momentum. For using it, one has to xnow
the thickness S** of iost momentum and ihe thickness V of di3pia-
cement. If, in their computalionp ihe velocity profile in the boun-
dary layer is assumed to be that of a plate, one obtains the appro-
priate expressions
S d
PO (22)
where (RW
1 2 +
kC I/-- ~k,)2 + (k'.), Wi)
Uj
-b!L -%
Card 4/8 PO

2 90
S/043761/000/004/005/008
Turbulent boundary layer of ... D274/D302
and + :a2 + 1 1 + (2-3)
U2 kl~ -2
V, - u
If the influence of the longitudinal pressure gradient is taken in-
to account, then K
orciln it
U8 k
1) k e u (2.6)
k2
Fa vW kt PO
U U1
where a
.U=- HW H,.
(H. + d
A
Determination of friction law: In order to find the friction lawp
i.e. the dependence of ~ on xp the equation
1 d (rF-PoU 28 **) + Pou Lu Tw (3-1)
Card 5/8 rF_ dx dx
agn -ye~
;RM

2)027
S/04 YD 61/000/004/005/008
Turbulent boundary layer of ... D274 302
is used which expresses the momentum law; a 0 for an airfoil and
1 for an axisymmetric body. One obtains
V u din r' (3.2)
U --I-P.
+ 4- 7 -,6- T,
;/-X- p a P- V_ p-,
where
N ub"== ft R**
P- -I- T--
This equation is solved by the method of successive approximation.
Setting
D Ll 1 fi(x), k arc8in
k2 2 f2(x)l
PO
one obtains 1n F- R ln f (3-3)
o3 1(x) + 5f2(x)'
For the determination of Z = Po/p OD R**9 one obtains
Card 6/8

29027
S/043/61/000/004/005/008
Turbuient boundary layer of D274/D302
ZIN-1 dz Z", + V _L,_ d In 1~ (3-4)
U - '~*' u' dx
where (X) n, _!Lf",-1f 2e-n, Nv
V_
If 6*/6*1 is considered as a known function of x, then Eq. (3-4) is
a linear differential equation whose solution is
F, (x) dx C+ F2 (x) e1 PI (X) dxd (3-5)
Z", ~= e X1
In the case of a :C~~ e ul, =-O),- one obtains for the friction coef-
ficient
47- 2 1- ZI I-
Cf - 2 1 1 it PO (3.6)
2
(Orcsind a. 1-n,
2k*'e - ( i - ~2) 7n*
VO U k2 PO
1,0
Card 7/8

Turbulent boundary layer of ... D274YI)302
h
if 110/11W h0/Hw then
(3-7)
k (arcsin Z)4
Ut U2)
Cf = 2ARI e k-) - ' (D !-)
VO k2 U
There are 3 Soviet-bloc referencee.
2)027
S/04 61/000/004/005/008
Card 8/8

GINZBURG, I.P.; KOCIIERYZHlMGV, G.V.
Turbulent boundary layer of a thermally inBulated wing or
axisymmetrical body. Vest.ILU 16 no.19:115-121 161. (MM 14:10)
(Aerodynamico)

An xr. 936-5. io ame
P;URBULn- NT BOVNDARY LAYER ON THERMALLY NONINSULATED WING
and G. V. Kocheryzhenkov. IN: Leningrad. Universitet.
Vestnik, no. 7: Seriya matematiki, mekhaniki i astronomii, no. 2, 1963,
86-96. S/043/63/007/002/003/008
An approwxdinate solutipn is presented of the problem of a turbulent boundary
-layer on a thermally noninsulat.ed wing or an axisymmetrical body in compres -
sible hypersonic flow. The method is based on two previous papers and requires
the assumption. '~-,he,.the"veldtity'depeiidence 6f tbt'al enthbLIpy in the t U rb u I e n t.
tecrion of 'the laoundaky layez! and -in the laminar sublayer can be expressed as a
qupLdratic function of v., in the form,
H-A + Bv,, + CV2 idthe turbulent region, and
2
H Hw + B V V.. irf the laminar sublayer.
1 :4 C1
Card 1/2

AID 11r. 986-5 10 June
TUMLMML 'BOMIMARY IXM (Coat 1d] 6/043/63/007/002/00j/CO8
7-'
tween friction stress
Ine velocity profiles are determined,'the relationship be
tV and I~hiakness of momentiza loss b-";: is described, and expressions Ior drag
and local s1kin friction coefficient are established, The calculation procedure is
out-lined for s. numerical example of a sp:aerical body with a radius of 20 cm in
an air f3low o.-NM = 20 with stagnation point-temperature Too -x 7000'. The .rev
sults ar,eplo#~4in,Xrap4s'.' (ANBI
-, 4-2 V R-N

LIKOVi, A.V., akademik, red.; SMOLISKIY, B.M., doktor tekhn. nauk,
prof., red.; GINZBURG,-jP., doktor fiz.-matem. nauk, prof.,
red.; ZABRODSKIY,_9_.'S_'., doktor tekhn. nauk., red.; KONAKOV,
P.K.P doktor tekhn. nauk, prof., red.; KOSTERIN, S.I.,doktor
tekhn. nauk, prof., red.; SHULIMAN, Z.P., inzh., otv. za
vypusk; KORIKOVSKIY, IA.,, red.; LARIONOV,.G.Ye., tekhn. red.
(Heat and Mass transfer] Teplo- i massoperenos. Moskva, Gos-
energoizdat. Vol.3.[General problems of heat transfer) Obshchie
voprosy teploobmena. 1963. 686 p. (MIRA 16:6)
1. Akademiya nauk Belorusokoy SSR (for Lykov).
(Heat--Transmission) (Mass transfer)

r Lr-~~ KouREHYMENROV, G.V.
GINHURG,
Turbulent boundary "Layez, rf a nonthermally Inaulated wing or
axisyarnAric body In a compreasible fluid. Yest.1LU 18 no.7z
8(-.98 163. (KMA 16 j 4)
(Aerothermr,dynamics) (Boundary layer)

VERESHCHAGINA, L.I.; GINZBIJRG, I.P., prof., rukovoditall raboty
Base pressure for solidn of revolution in a-uperoonic gas flow.
Vast. WU 18 no.13:139-143 163. (MIRi 16,9)
(Aarodynamicn, Supersonic)

ACCISSSION NR: AP401,/,1,16 S/0170/U./000/006/WWW74
AUTHOR., Ginzburg, L P.
TITLE: The relationship between heat content and velocity in the bounetary layer
of flowing gas
SOURCE: Inthenerno-fizicheskiy zhurnal, no. 8, 1964p 64-74
TOPIC TAGS: boundary layert heat transfer, Prandtl number, laminar flow,
turbulent flow, Lewis ntuabor
ABSTRACT: An approximate relationship between heat content h and flow velocity
V
for arbitrary values of Pr in turbulent as well as in physical flows was
X
established using the boundary layer equations in Crocco variables, On the
assumption that Lei = 1 and ejt~ const in the boundary layer,, general expressions
are derived for the coefficients R( and S
1/4
,Card

ACCESSION UR: AP4044416
S 1) Prexp I-pr as d d
Pr(O) dip
R (V, t)2 prexp(_~(J-pr) do d
dip
I -Pr CIO
exp d d V1.
0 uhere v./u. W Y, and for
w
1, R be:omes tho recovery factor. The values of R(1,� ) and S(If ) aro then
doterndned for laminar boundary layors-
S (1) Pr-/,, R (1) - VPr.
turbulent boundary layerp assuming a sublayer
S110- Pr.' 11 -- (I - p.r..T.'I' R (1)10 - PrA) VIA
,-turbulent boundary layers assuming Un-Driest's three-layer G:Pproximationj and
Card 2A
Mai

-MMMMIR., AP4044416
-7*ImAPaez,t jONgdff7 layer v:LlMt -V~z ---Amw-mPiAAPA'IV of SMANdoft and
V= taikow. Fins ily, 5 and R-are sacianted for Pr I iuLth the rexult
S +
Pr,
+ Pr, r(wjr(in)
It (1) pirqp Prif.+ Vr,~ (Pr,)
Pr. r qw, + 1 /3) where
for Pr I in the presence of flow
injection at the wall the values of R and 5 take a modified form given by
S (i)
Pr,,
R (1) - R (T.) + (I - These results show the effect of Pr
(turbulont and lwainar) on he"A transfer to the walls from the boundary layer and
establish a relationship between h and vxe Origo art. has: 66 formulas and 2
figures.
Car.d-13A

ACCESSION NRt AP404W6
;I ASSOCIATION: Gooudarstvenqy*~r univeraitat im A. A. Zdanova g. Leningrad
(Leningrad State Universit.
v)
SUBNITTEDs 22Nov63
ENCLs 00
SUB COIE: MEqTD
NO REF SM 005 OTHER s 000

GIIIZBURG, I.P. (Leningrad)
"On the solution of problems of the turbulent boundoxy layer in a
compressible fluid-gas mixture".
report presented at the 2nd All-Union Conarss on Theoretical and Applied
a -
I-Ilechani-cs, Moscow, 29 Jan - ~ Feb 64.

Pd-;,-P;,_4 A F-ETIR/
-6
AFWT
AEDCf%n),/ASDI'f)/BSD/SSD/AS(mp)--2/4SD(4)/AFT~G(a)/ESO(gz)/ESD(t) RM
:ACCESSION NRt AP4044459 S/0043/64/000/003/0089/061
:AUTHOR: Ginzb I P koch~ery*zhenk:o G dyf:.nova
A turbulent boundary layer on a pemeable plate
~SOURCZI Leninarad. Universitet. Vestnik. Beriya matematiki., mek-
:.haniki I "'Ciiiiomfi, no, 3, 1964, 89-102
~TOPTC TAGS* turbulent boundary layer, boundary layer permeable
"plate, mass transfer, heat transfer, skin friction. diffusion, com-
~prassible gas flow
a
tABSTRACTt The effect of mass trisnafer an compressible, turbulent-
:bounddry-layer skin friction an.4 on heat transfer when mass is inject-
.ed into or withdrawn from the layer normal to the surface Of a P.Orme-
able plate is studiedfor arbitrary constant Prandtl and Lf)wlis num-
bers. Investigations were carried out on the basis of a a'emiempiri-
cal theory of turbulence by means of a two-layer method proposed by
1. P. Ginzburgg Steady flow of a thermodynamically ideal gas is con-
sidered in the presence of diflusLon and in the absence of inertial
forces, heat emission, and chemical reactionss The effect of thermal
;'diffusion is neglected. [formul-38 expreasing relations between total

L8826-65~-
;tACCESSION NK: AP4044459
..enthalpy and velocity, mass cancentration of the components of a bin-
.ary mixture and velocity, and: shear stress and layer thickness are
~derived. Expressions for detormLning velocity and temperature pro-
files and evaluating the effect of injection on the skin-friction
coefficient are established. The resulta of calculation made by this
method agree with available experimental data. Orig. art. hasi I
figure and 60 formulas.
ASOOCIATION: none
SUBMITTEDo 03Jurt.63 ATD PRESS: 3100 ENCL: 00
SUB CODEt HE, AS NO RYF SOV: 007 OTIEERt 000

GIN21BUR6, 1. P.
"Methods of solution of' turbulent boundary layer problem, for a inixture of'
gase- "
rcport submitted for 2nd ALL-Union Carif ori Heat $e. Mac.; Traiuffer, Mimk, h-lp
May 1964.
Sci Res Inut of' M.-atherrvitIcs & Mcchmlir,%, Leningrad Stat.e Univ.

GI'NZBURGY I.P.
Relation betvreon the enthalpy and velocity of a gas moving, in a
boimdary layer. Inzh.-fiz. zhur. 7 no.8:64-74 I/ Ag 61,. (141ILk 17: 10)
1. GosudarBtvennr,, univeroitat im. A.A. Zhdanova, Laningrad,

I
I
VALLAND-"R, S3,; GINz"DIN, 1J'.; POLYAKOV, N..; VJS1,10", P.P.
-,-. . I - - 9 - 11 . I H .
Konstantin Ivanovich Strakhovich, 1905- ; on his 60th birthday.
Inzh.-fj.z. zhur. 8 no.3:409-410 Mr 165.
OMIRA 18: 5)

L 5153-66 EWT(I)/EWP(m)/EWT(m)/Ft4P(w)/EPF(c)/LTC/EPF(n)-2/BWG(m)/F.WA(d)/
T7E-'dP(t)/FCS(k)/r,,WP(b)/LWA(l) JDIWWIDJ
ACCESSION NR: AP5020937 UR/0170/66/009/002/0165/0162
632.617.4
77
AUTI1011- Ginzburr, 1. P. - Korneva, 1. V.
TITLE: The effect of the turbulent number Prt on the friction hQjttranafer of a plate
in turbulent gas flow
SOURCE: Inzhenprno-fizicheBldy zhurnal, v. 9, no.2, 1965, 155-162
TOPIC TAG-9: Mcdon coefficient, heat tranafer, plate, turbulent flow, gas flovf, Prandtl
number
ADSTRACT: 71lie following expression was obtained elsewhere (Glnzburg, 1. P. IFZh,
No. 8, 1964.) to determine the relationship between the heat content and flow rate in the
case of nongradient flow at arbitrary Pr and Prt (where L andY are laminar and turb;i
L
flow, respectively):
Card 1/3
R

L 5155-66
ACCESSION NR: "5020937
where
exp.- dy d1pi
N) 2 exp dp Pr qxp x
X OlPr - 1)dT dy)d(P19 a)
W ftm AM -h1jj, 0/211,.'
IU
The present 'authors use this expression and the basic premises In tho acralempiric theory
of turbulence to evaluate the effect of tho PrV number on the friction and heat transfer
loefficient of a plate. Orig. art. has: 18 numbered formulas.
Card 2/3

26851
vl~ I ~- L-
AUTHOR: Ginzburg, 1. PO;
)/ETC/
SOURCE CODE: UR/0170/65/009/004/0444i&~07
'V Y, 5,57
Krestlyaninova, N. S.
991
ORG. State University im. A. A. '&anov, Leningrad (Gosudarstvennyy universitet)
TITLE: The turbulent boundary layer on a plate in an incompressible fluid with
blowing of a substance
SOURCE: Inzhenemo-fizicheskiy zhurnal, v. 9, no. 4, 1965, 444-450
/I S-5- 1, e1;1' '.' ."-
TOPIC TAGS, turbulent boundary laye , heya-t transfer, incompressible flow,
Reynolds number
ABSTRACT: The effect of blowing on surface friction and heat transfer in the case
of a turbulent boundary layer has been treated previously. To solve the resulting
euqations, certain supplementary assumptions were made as to the thickness of the
laminar sublayer or as to the velocities at its boundary. The present article consi-
ders the effect of blowing on the parameters of the boundary layer and on friction,
on the basis of the two-layer scheme of the semiempirical theory of turbulence.
To confirm the validity of the limiting (boundary) laws proposed previously, and to
simplify the calculations, the present article considers the case of an incompressi-
ble fluid. The article develops an approximate numerical solution of the basic equa-
1/2 UDC:532.517.4

L 78
ACC NM 'AP5026851
0
tions. The dependence of the relative friction coefficient on the blowing parameter
is shown in a figure. The results calculatedby the proposed scheme, with a finite
Rex number, are shown to be closer to experimental results than tile results of
previous work. In the limiting case when Rex approaches infinity, the results
coincide. Orig. art. has: 25 formulas, 3 figures and I table
SUB CODE: ME1 SUBM DATE: 18Jan65/ ORIG REF: 005/ OTH REF: 002
1
61P

OIINZBURO~ I . S' I
"Chronic Ulcerative Ginrivitis," Stomatologlya, No.1, 1952

GINZBURG, I.S., dotsent, kandidut raeditninakikh nuuk; NOVIK, 1.0., dotoent, zave-
Idupiahchiy; GORCH"OT. A.K.. profenoor, direktor.
Pathogenic therapy of ulcerative stomatitis. Stomatologila no.4:10-15 Jl-
A9 '53. (KLU 6:9)
1. Xafedra torapevticheakoy stomatologil Kiyev8kogo rneditsinskogo stomatolo-
gicheskogo inntituta (for Novik). 2. Kiyevakiy meditainskiy stomutologiche-
skiy institut (for Gorchakov). (stomatitis)

GINZBURG, I.S., ksndidat meditainakikh nauk
Role of vascular abangea in the periodontal tissues In the
pathogenesis of paradpntosis. Stomatologtia, no,3:12-16 Yq-J* 154
C' (HLRk 7:6)
1. Iz kafedry terapevtIchemkoy stomatologii(zav. dotsent 1.0.
lovik) I kafedry patologicheskoy A-tomii (xaY* prof, I.M. pays&-
Ichovich) kiyevskogo meditsinskogo stomatologichookogo Instituta
11r. Prof. A.K.Gorchakov)
(PAIODOW IUM, diseases.
*pathogen.. periodontal vase. changes)
(FARIODOETIUM. blood supply,
*vase. changes in pathogen. of pariodontomis)

GINZBURG, I.S.
Patbogeneels and therapy of hypertrophic gingivitis. Stomatologiia
no.4:63-0~ JI-Ag '55. ( MLRA 8:10)
1. 17 kaf"dry terapevticheakoy, otomatologii (zav.dotsent I.O.Novik)
Klyevskogo mnditninakogo stowitologicheakogo InBtituta.
(GLU-IS--DISMASES)

NOVIK, 1.0., prof.; GDIZ13UPG, I ..,-doteent (Kiyev)
--j,3 %
*Principles of the oathological aivitomy of the oral cavity and
teeth* by I.M. PeAsakhovich. Revi(,wed by 1.0. Novik, I.S. Ginzburg.
Vrach. delo no.4:431-433 Ap 159. (MIRA 12:7)
(STOMATOWGY) (PEISAKMVICH, I.M.)

GINZFURG, I.S.; NASIROT, A.B.
Some peculiarities In tho pathogenesis and clinical aspecta of
tuberculous lymphadenitle with an external and mosenterial loca-
lization. Azarb.med.zhur. no.2:-14-18 7 160. (KMA 13.5)
(LUMTICS-TUBIROMSIS)

VAYSBLAT, Solomon Naumovich, zasl. doyatell nauki USSR, prof.1
GJNZBURG, I,S... red.~ BYKOV, N.M., tekhn. red.
(Local anesthesia for operations on the face, the jaws, and
the teeth]Maatnoo obezbolivania pri operatsiiakh na litse,
cheliustiakh i zubakh. Kiev, Goomedizdat USSR, 1962. 468 p.
(MIRA 16:3)
(WCAL ANESTHESIA) (FACE-SURGERY)
(JAWS--SURGERY) (ANESTHESIA IN DENTISTRY)
je

GIIIZBIJPGI I.S. prof., zasluzhennyy deyatell nau~i4 KAFAROV, K.I., aspirant.
Phlegmon in the newborn and infants during the first year
of liTe. Azerb. med. zhur. no.10-3.1 Ja !62. (MIRA 1615)
1. 11 %afedry II gospitallnoy i detslcoy khirurgii pediatriches-
kogo fakullteta (zav.-prof. I.S.Ginzburg) Azerbaydzhanokogo go-
sudarstvennogo meditsinakogo instituta imeni N.Varimanova (rektor
zaslu*henn-yy deyatell nauki, prof. B A. Eyvazov).
(WIVEGTIVE TISSIJE&-DISFMES) iMAPTS-DISEASES)

GINZMRG, I. S. (Kiyev)
Some characteristics of paradentium vancularization and its
clinical significance Probl.stom. 606-41 162. (MIRA 160)
iGUMS-BLOOD SUPPLY)

NOVIK) Isaak OBipovich, prof.; GINZBURG, I.S.v red.
(Periodontosis; pathogenesiso clinical aspects and
treatment] Parodontozj patogenez, klinika i lechenie.
2., ispr. i dop. izd. Kievt Zdorovvia, 1964. 325 p.
(MIRA 17t12)

BETELIMIANY Abram Isaa-kovich; I'OZDIIYAKOVA, Antonina Illa.-io.-wvna;
MUMINA, Apastasiya Denisovna; ALEKSAND.MVA, Yuliya
Mikhaylovna;_~_LNT2~8THPJ I.S.., red.
[Pediatric orthopedic stoirAtolofg] Ortopedicheskaia atoma-
tologiia det2kogo von-asta. Kiev, Zdorovlia, 1965. 406 p.
(MIAA 18:9)

~',7-7 1. S.
1. ,
Ginzhurr, 1. S. "Certain clinical-inol,pilololical peculiariticLi of c2accr af ti.c ;.:-;ujr,,ary
-tReport), Trudy III Zakavk;xzsk. zll-lezul.t ~1drarg,,)v, Yerevan, (or. clover:
Fl,,nd, " 1~
1949), P. 103-113
SO: U-52110, 17 Dec. 533 (LetoPis 'Zimmal In:j1di Statcy, No. 25), 191,J).

GINZBtMG, I.S., zaelushemayy dayatell nauki
Active therapy of precancerous conditions In prevention of cancer.
Trudy "M SSSR 21 no.4:88-92 152. (KLRA 10;8)
lo 1z nmuchno-imeledovateliskogo
I onkologfi AzGSR.
(NBOPIJSXS. prevention ani
ther. of precancerous
institute rentgonologii, radiologii
control,
cond.)

Cnr Vh) Z_ '15 J k I_r' I . ~z .
HADZHAROV. A.G., kandidat meditBinskikh nauk; AVMUKH, R.I.; GINZBURG, I.S., pro-
fessor, zuslushennyy deyatell nauki, direktor.
Tuberculosis of the stomach and duodenum. Khirurgiia no.7:56-61 JI 153.
(K6HA 6;9)
1. Azerbaydzhanakiy nauchno-imaledovatel'okiy institut rentgenologii, radio-
logii i onkologii. (Stomach--Tuberculoois) (Daodenum--%berculosim)

1; i 41:- 1,, 41. F~_i ,I . S . ,1;).Of .
"roll feraLAoris, Turaor Grcvth, rund of i tolic. t ive I
Pad Inc,tones." a
pr~- , M _" .
, serited oLL the TranEcaucanian Radiolor, L(,a). ,'',j I I ! n L, ~_ - 1 (4!,, ( L.
- .- -1, -
1,r.. l,'I.I;'( -1 I-r,
1 .1 1 1) -

USSR/General Proble'MO of Pathology - Twwrs. T-5
Abs Jour : Ref Zhur Biol., No 1, 1958, 3074
Author : Ginsburg, I.S.
Inst
Title Proliferations, Ttuwr Growth, and Tropism of the Radioacti-
ve Isotopes.
Orig Pub Tr. 1-y Zakavkazak. Konferentsii Po Med. Radiol. Tbilisi,
Gruzmedgiz, 1956, 245-252
Abstract No abstract.
Card 1/1