SCIENTIFIC ABSTRACT USTIASHVILI, A.D. - USTIMENKO, I.L.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001858220003-2
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: April 3, 2001
• Sequence Number: 3
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

USTIASHVILI, A.D.. professor; HADIPASUILI, M.D.
Effect of vulcanic mud from the Akhtala spa on ovarian function;
experimental morphological tind clinical findings. Akush. i gin.
no.LL..65-66 JI-Ag 154. (KIRA 7tll)
1. Iz Nauchno-issledovatel'okogo instituta kurortologii i fiziche-
skikh motodov lecheniya (clir. kandidat maditsinskikh nauk V.G.
Gogibedashvili) Kinisteretva zdravookhraneniya Gruzinskoy GSR.
(OVARIES, effect of drugs on,
inud ther.,* clin. & exper. findings)
(MUD TMMAPT,
off. on ovaries, clin. & exper, findings)

USTIASHVILI, A.D.
[Rh factor in obstetrical Remus-faktor v skusherstve. Tbilisi,
Sabchots Sakartvelo, 1958. 18 p. (MIRA 13:5)
(RH VICTOR)

USTIGH, A.F., starshiv elektromakhanik
%I I -OW, im-MAAAA6rdrk*;I.
Ve need smaller electric wiring diagramB. Avtom. telen. i sylaz'
2 no.9:41 3 158. (MIRA 11:10)
l.Mineralovodskaya distantelyu signalizataii i avyazi Ordzhonikidzevsko3r
dorogi.
(Electric wiring-Diagrams)

__sli~rshiy elektromekhanik; KMZF
USTICH, L.F.-, W, M.N., starshiy
CHEPELEVICH, M. 1'.
From the editord mail. Aitom... telem, i Bviaz' 5 no.3:44 Mr
161. (MIRA 14:9)
1. Mineralovodakaya distantsiy96signalizatsii i avyazi Severo-
Kavkazakoy dorogi (for Uatoich). 2. Nadozhdinskaya distantsiya
aignalizatsii i avyazi Svordlovskoy dorogi (for Knyazov). 3.
,nalizataii i avyazi Litovskoy dorogi,
Nachaltnik laboratorii sig
(for Chdpelevich).
(Railroads--Electric equipment)
(RaUroads--Corumnication systems)
(Railroads--Signaling;Pwltiterlocking systems)

BIMG, F.P.; FZYGILISON, B.Tu.; Prinimali uchastiye: ZABETSKIT,'G.F., inzh.;
RAKMH, Y.G., inzh.; KLrZMSOV. re.I., inzli.; SKOSYREVA, A.H.,
starshiy te)dmik; qSTIOSM, R.D., starshly tek.Wk.
Metal shell molds. Lit. proizv. no-10:32-33 0 16o. (MIRA 13:10)
(Youndaries-Equipment and supplies)

DOLWTp F.Z.j1,WTIC=KOL-j+
Combined batch for dolomite and dolomite-magnesite refractories
with free lime, OPSUPor)' 25 Ao.Ils523-525 160, (KERA 13:12)
1. Ukrainskly naucbno-isoledovatelinkiy inotitut opouporovo
(Firebrick) (Binding materia3s)

DOLKART, F.Z,. Prinimal uchastiye USTICHENKOt_V.A.
L_
Characteristics of refractory materials -nade of calcined
dolomite on a resin balse. Ogneupory 26 no.1:329-335 161.
w ,
I . . . (MIRA 107)
10 Ukrainokiy nauchno-iseleddvatellskiy inotitut ogneuporov.
'(Dolowite)
(Rofra4tory materials)

(.,0!7 1. a)
Dp t e c f
eloctric modeling
in . 5 -.2 1-2!~ 165.
tl,f~
;l:;ch.coor. 7
Instaill (MIRA 18:
10)

VOLOSHINY A,M,, inzh.; PANFILOV, I.D.j, tekhnik; USTIMENKO, A.A., tekhnik
Ventilating a mine section with the collector-drift in
the hanging wall of the ore body., Met, i gornorud. prom*
no.4:76-77 JI-Ag 163. (KMA 16:11)
1. Rudnik im. Dzerohinakogot Krivoy Rog.

USTIMMKO, A. S.
Cand Agr Sci - (diss) "Effect of mineral nutrient and ;rrowin,7
conditions on the productivity of above-surface and root mas-Ses
of perennial grasses." Belaya TserkovI 1961. 20 pp;(Ministry
of Agriculture Ukrainian SSR, Belotserkov' Agricultural Inst);
200 copies;price not given; (KL16-61 sup, 233)

j JP
_KCd NR, AP6023750 SOURCE CONE: UR73-fi~g-/66-i-ooo/003/0124/'0134-----I
AUTHOR: Ustimenko B. M Ibragimov, I. I.; #urj~~n E~.
LA
ORG: none
TITLE: Experimental study of temperature profiles in a swirling nemiconfined
turbulent jet in a concurrent flow
SOURCE: Alma-Ata. Kazakhskiy nauchno-isoledavatellskiy institut energetiki.
Problemy teploenergetiki i prikladnoy teplofiziki, no. 3,1966, 124-1311
TOPIC TAGS: incompressible liquid, turbulent jet, temperature profile, velocity
prpfile, concurrent flow, semiconfined turbulent jet
ABSTRACT: Results are presented of an expezimntal.study of the t rature distri-
bution inaswirling turbulent jet of an imcompressilbe liquid"pro gating along a
cylindrical wall both in the presence of a concurrent Ilow and without it. Both
symmetric and asymmetric boundary conditions are considered. The effect of the
parameter m = uf/ui (where uf and uj refer to the velocity of the main flaw and the
jet, respectively) and of the vortex on the jet boundaries, temperature profiles,
and the jet attenuation intensity was determined using the previously described
experimental unit (Ibragimov, I. I., Ustimenko, B. P., Izvestiya Akademii Nauk Kaz.
SSRP seriya fiz.-mat.nauk, 1964, no. 2) with swirl vanes. A comparison of the
experimental relative maxinum temperature profiles, the excess temperature profiles,
Card 1/2

L 38843-66
ACC NR, \AP6023750
and the .velocity profiles in various cross sections
of the jet showd the presence of flow self-modelling and a similarity in the exces
temperature and velocity profiles in the jet cross sections. With increasing
m para ter, the maximm excess terperature in the jet dmWed rapidly and the
relative thermal boundaries of the jet underwent contraction. The presence of a
vortex leads to an expansion of the jet boundaries. Orig. art. has: 1 table and
11 figures. (PSI
SUB CODE: 20/ SUBM IDATE: none/ ORIG M': 007/
C,.d 2/2

USTlYMNO, B. P.
"Investigation of the Aerodynamics of a Stream in a Furnace Cyclone Chamber."
Cand Tech Sci, Power Engineering Inst, Acad Sci. Kazakh SSR, Alma-Ata, 1954.
Whlsfekh, 11ov .54)
Survey of Scientific and Technical. Dissertations Defended at USSR Higher
Educational Institutions (11)
SC: SIX1. 110. 521, 2 Jun 55

VULIS, L.A.; USTMNKO, B.P.
"
Aerodynamic diagram of current in a cyclone cbamber. Yest.AN Xazakh.
SSR 11 no.4:89-97 Ap '54. (XTRA 7:3)
(Aerodynamics)

5490. - Wm- Vulll. L-A ald
u3tlw~ (Tcpjocna*gtt9La (Vicat P&- Zngng, tio3cim), 1954, vol. 1,
Ucl,.ntk, Jum 1555, vcd. 5, 265-2-10)- The-
'r ml, (I
a* an The
In cycao'no fwn.,cc climbers, lhr~. ncvcUnt of We Jt, A
-~trbulcnt nixtr's plxxes3 In UP cyolor~o &ov '0~- and 'be wst affleftnt ac-Uwel
of Injc0ting CCMbmtIvn Or riv otolml. A :,crcrollzcd gqtiatlcn tcr flow In
the cyclone la presenW, (I M.F.P.

-----------
-1 -7
AID P - 4364
Subject USSR/Heat Engineering
Card 1/1 Pub. 110-a - 9/19
Authors Vulis, L. A., Dr. Tech. Sci. Professor and B-,, P.
Ustimenko, Kand. Tech. Sci. Power Institute of the
Kazakh ademy of Sciences
Title The influence of a non-isothermal field upon the flow
aerodynamics in a cyclone type furnace chamber.
Periodical Teploenergetika, 4, 36-39, Ap 1956
Ab~tract The problem of applying data pertaining to the aero-
dynamic properties of a cold air flow in a cyclone
combustion chamber to the non-isothermal motion of a
gas flow in the same type of furnace. Three diagrams.
Seven Russian references, 1953-1956.
Institution : Nwe k~,J_ c(lol-T, Jkc"~:) _j
Submitted : No date

UST1140KO, B. P.
1#On AutcmOdehng Motion of Pluid In a Ideakly Twintea Stream,"
by B. P. !Ustimenko, Izvestiva Akademii Nauk Kazakh SSR, Serlya
Energeticheekaya, No 11, 1956) PP 111-121
Work reviews previously published solutions to the problem of wenkl,v
tvisted streams solved by the method of the asymptotic reonlution of ve-
locities and pressure into series along negative degrees of the radial
distance from the source of the stream. It Is shown that these same so-
lutions (first approximation) may be found by the simpler automodeling
solution method, i.e., the method so well-proved in nontwisting streams.
The work presents the solution to the previously uninvestigated prob-
lem of the distribution of heat in a nonisothermic, weakly twisted radial-
aperture stream.
a S'9

SOV/124-58-7-7718
Translation from: Referativnyy zhurnal, Mekhanika, 1958, Nr 7, p 58 (USSR)
I
AUT'qOR: Ustimenko, B.P.____
TITLE:--' On the Self -similar Motion of Liquid in a Slightly Twisted Jet
(0b avtomodellnom dvizhenii zhidkosti v slabozakruchennoy
struye)
PERIODICAL: Izv. AN KazSSR. Ser. energ., 1956, Nr 11, pp 111 - 12 1
ABSTRACT: The author describes the existing solutions of the diffusion
of twisted axial and radially- slot- shaped jets in a space con-
taining the same liquid and directs his attention to the self -
evident fact that the first terms of the asymptotic expansions
of the solutions according to the inverse powers of the dis-
tances from the source correspond to the so-called self-
similar motions. At the end of the article the solutions of the
corresponding nonisothermal problems and the well-known fact
of the similarity of the velocity and the excess -temperature
fields, when the value of the Prandtl number is equal to unity,
are confirmed.
1. Liquids--Motion 2. Jets--Properties L.G. Loytsyanskiy
Card 1/1 3. Mathematics--Applications

U0 I I M
5(l) 3 6 PHASE I BOOK M(PLOITATION
Akademiya, nauk Kazakhokoy SSSR, Alma-Ata
SOV11659
Issledovaniye fizicheskilboonov rabochego protsessa topok i peehey
(Investigation of the Ehysical Bases of Operational Processes of
Combustion Chambers and Furnaces) Alma-Ata,, Izdat AN Kazikhakoy
SSR, 1957. -369 p. 8oo copies printed.
Additionial Sponsoring Agency.: Alma-Ata. KitzakhskJLy gosudarstvennyy
universitet, im. S.M. Klrova.
Zd, (Title page); L,A, VWUs, Doctor of Technical Sciences, Profes-
sor; Ed, (Inside book): D.M. Glazyrina; Tech. Ed.: Z.P. Rorokina.
PURPOSE: This book is intended for a wide circle of scientists &7jd
industrial engineers.
COVERAGE: The twenty-nine articles of this collection report on
experimental and theoretical investigations of different physical
Card ~/7

Investigation of the Physical (Cont.) SOV/1059
phenomena which constitute an integral part of the complex
operational processes of modern combustion engineering equipment,
and also, the entire process applicable to different types of
burners and furnaces (cyclone combustion chambers, muffle'burners,
burners with automatic stokers, etc.). Articles in Part I treat
laminar and turbulent jets of liquids and compressible gas. Part
II reviews methods of modeling combustion processes (lightp hy-
draulic and electrical), enthalpy, temperature me - calo-
rimetry, etc. Part III relates to different problems and theories
of fuel combustion and special operational features of combustion
and furnace equipment. No personalities are mentioned.
TAKE OF CONTENTS:
Foreword 3
From the Editor 5
Card 2/7

Investigation of the Physical (Cont.) SOV/1659
PART I* THE AERODYNAMICS OF JET FLOW
Vulis, L.A. Jet-flow Problems of Gas Dynamics 15
Kashkarov,, B,P, Some Accurate Solutions in the Theory of Incom-
pressible Liquid Jets 54
Ustimenkol B.P. The Investigation of Slightly Involute Jets 64
Vulis, L. A4, V.P. Kashkarov, and T.P,, Leantlyeva, Investiga-
tion of Complex Turbulent Jet Flows 1 86
Vulls,, LoA,j and Sol. Isatayev. Turbulent Flow of an Incomp;qes-
sible Liquid in the Wake of a Poorly-streamlined Body 112
Terekhina, N.N. Propagation of a Free Turbulent Gas Jet 125
Vulis, L*A,, T,K, Mironenko, and N,N, TerekhIna. Approximate
Calculation of Speed and Temperature Distribution in Free
Turbulent Jets of Compressible Gas 14A
Card 3/7

Investigation of the Physical (Cont.)
SOVI-1659
Kashkarov, V,P, The Question of the Flat Boundary of a Com-
pressible Gas Jet
Bukhman, S.V., and A.P. Chernov. The Investigation ~f Two-
Phase Free Jets
PART II. METHODS OF INVESTIGATION AND MASURING
V`ulisp L,A,,, and V.G. Klinger. Investigating Radiant Energy
Exchange by a Method ZWloying Light Models
Klinger, V.0. Experimental Investigation of Radiant Energy
Exchange by an Method Employing Light Models.
Vulls, L.A, The Use of Hydro Integrators (Hydrodynamic and
Hydrostatic Integrators] in the Solutions of Some Prac-
tical Problems
Potseluyko, V.A., and A.T. Trofimenko, The Investigation of
a Temperature Field by the Electrothermal Analogy Method
Card 4/ 7
166
175
193
211
223
242

Investigation of the Physical (cont.)
SOV/1659
Vulis, L.A., N.D. Kosov, and V,A, Potseluyko, Determining the
HbW Constants of Poor Heat Conductors
'YdovAnko, X.I., and V.V. Favorskiy. The Temperature Charac-
teristics of Some Kazakhstan Coal Ashes
Kosov's NO. Some Methods of Determining the Diffusion Coef-
f1cient of Ganes 4
Kosov.. N.D. The Temperature Dependency of the Diffusion Coef-
ficient of Gases
Basina, I.P. Methods of Measuring Flame Temperatures in Sm6lt-
Ing Furnaces
Vulis, L.A., and N.D, Kosov.
Measurement
A New Method of Calori6etrie
252
279
285
291
297
311
Card 5/1

Investigation of the Physical (Cont,) SOVI-1659
PART III. COMBUSTION, COMBUSTION CKAMBVJ AND VMACW
Vulis" L.A. Synopsis of the Elementary Theory of Heat Condi-
tions During Combustion
Favorskiyp V.V, Some 4ecial Features of Ach Coal Combustion
Rezn~akov., A*B, The Burning of a Pulverized-Coal Flame
Leontlyevap T.P. The Aerodynamics of a Muffle Burner
Vulls, L*A,,,, and B.P, Ustimenko. Investigation of the Aero-
dynamics of a ~E_;yalone V=bwrtion Chamber
Tonkohogiy, A,V,j and I,P* Basina. The Burning and Separation
of Fuel Particles in a Cyclone Combustion Chamber
Teplitskiy,, N.G. The Sharp Blast in Combustion Chambers
Tonkonogiy, A.V. The Choice of Burners for Reverberatory Cop-
per-Smelting Furnaces
Card 6/7
321
345
361
380
389
407
420
428

Investigation of the Physical (Cont.) BOV11659
Tonkonogly,, A,V.,, and I.,P* Basina, The Burning of Coal With
a High Content of Ash In a Cyclone Combustion Chamber 447
Favorskiy,, V.V* Some Results of the Study of Working Prinei'
plea of Combustion Chambors With Stoker Orate* 457
Supplement (From the Editor) 468
AVAILABM: Library of Congress
Card 7/7 TN/;ob
~5-28-59

8(6%,
S07i I!- -5?-4-~-547
Tr an s I a til~,-u fr~srn: Re fera-tlvayy zzlav. _~~.a, . E I
AUTHOR: Vulie, L. A. , and Uctirynenlc, B. P.
TITLE: 1--vestigation cf taa Ae_-Ddy-.a_nmic9 of ~_: 'Clyclone
PER20MCAL: V sb. fiz. osnov. r~.bcchego
Al.ma -Ata, AS Kr-- zakhekaya SSR. 1957, wo 389 -406
ABSTRACT: A theoretical 2.nd expeximental i:r:,reetij.Uio-a c~f '~Le a
C-felcme combuistor hzF. bec-a niade o-n c-,Id of -1 cy,:'_~,ne -C~.Jef
atte-~at.;,:;.a was na-M t-- the movemen! z:,f a siltgle-ph~lae ga-~
jet Ymt-i-a iz presentul'. Evps-nIms-ato are dascribedl oa -L-r,a v~,t
diflerea' vallues o.' -oz.~-axne'.EZ5; the zlz! o-Innitte,! thx~,.igh "'%e o c~ -.z 1 e t
Znd mix-'nag ti,-e d:~agged into the '&hT:3-_-_,Wh 1:11S by 1 E V E e
curre,--t& beei-i studied. On the basis of V~-._- resultu -at atirn:7,umate
anz!-;tiu~l of t-he turbulezit mix.;ng in the combaz~"O_- in, The
pro'ble-n-1 Cf rationp-1 ad'mi3Eian is considered. An i..-, tl~.e r~_,n-ibem of
tangential aiz -Laletp, sit-aated the combtist-,)r perf.metc-_ ~Ie,- e~~.efj
Card 11Z

SOV! 1 17-51-4-651
investigatiom of the Aerodynamics of a Cyclone Combuator
the combustor resistance and raises the relative vortexing (1he rat;:, n," tile
tangential speed in the combustor to the inlet speed). Thus, whea he
speed changes from 134 m/sec (air adm ssion through cne nozzle' t-~ 4 3 n. LAE
(air admission through four nozzlea), the total combust3r resistance drcp,-;
iesb t'han one-third (from 1,640 to 520 mm water collum-n'; the
I"he tangential speed even slightly increases. The possibility of eKtendLnP_, t)'~c
ynamic blowouts of the cyclo-ne charnber Over to
res~;,.Its af cold aerod,
.sothermic motion of the gas stream in a real combustoz7 is analjie.~; `-e
influence of gas-temperature variation at the cyclone entrance upr_n t,_"'e
and circular speed components is evaluated, as well as the ir-fluence cf -%.',--e
temperature cross gradient in the cyclone upon the above comp.=en.3. The
ds-ta in the article can be used both for designing cyclone combu s t 1~ ! S
developing a theory and method for computing the working proce!B-_
Card 2/2

83645
/Z ~'Y,3 0 S/123/59/000/007/014/014
6, .2 1,3,5- A004/AO01
fia'nslation from: Referativnyy zhurnal. Mashinostroyeniye, 1959, No,~ 7,
P- 355, # 27250
AUTHORS: Vulia, L.A., Ustimenk o,--B.P
TITLE: Investigating the Ae odynamic7 of Cyclone Combustion Chambers
PERIODICAL: V sb.; Issled. fiz. osnov. rabochego pi-otsessa topok i pechey.
Alma-Ata. AN KazSSR, 1957, PP- 389 - 406
TEXT. The explanation of the phenomenon of the gas flow motion in
the cyclone chamber is based on the idea of a rotating turbulent hollow
jet. Such a jet, with a border layer directed to the chamber axis, drains
masses of air, which flow into the zone of reverse currents, and puts them
into rotation. The intensive turbulent mixing within the inner zone of
the chambercan be assumed as the basis of the mechanism of motion. The ori-
gination of an axial zone of reverse currents can be explained by the turbij..
lent exchange of the moments of momentum, which causes a pressure drop over
the length of the chamber. This conception wE.s confirmed by experiments
Card 1/3

83645
S/123/59/000/007/014/014
A004/AO01
Investigating the Aerodynamics of C:rclone Combustion Chambers
made on two cold models of the cyclone chamber in order to study the mix-
ing of the main and the counter air flow brought into the chamber by re-
verse currents. The tests proved the presence of a self-simulating motion
in the temperature field. The nature of the relative temperature change
in the cross-section of the cyclone is similar to the profile of excess
temperature in the free turbulent jet. The diagrams of the lines of con-
stant concentration of the primary air present a descriptive picturo of
the mixing of the basic and counter flow of air. They make it pos8ible
to evaluate the effect of the various structural changes and to obtain an
idea of the fire operation of 'the chamber. The authors found an approxi-
mate analytical solution which corresponds to the accepted physical layou
and, regarding the quality, reflects the structure of the flow correctly.
During the experiments the authors detected the favorable effect of air
Inputs, distributed along the perimeter of the chamber, since,ill, the num-
ber of tangential inputs is increased, the resistance of the chamber drops
abruptly and the relative vortex within the chamber grows. An analysis
of the effect of the anisothermal property of the temperature field on the
flow aerodynamics in the chamber shows an increase in the axia component
Card 2/3

83645
S/123/59/000/007/014/014
A004/AO01
Investigating the Aerodynamics of Cyclone Combustion Chambers
and the invariability of the tangential component of speed relative to any
cross-section of the chamber, and the comparatively insignificant effect,
under concrete cyclone conditions, of the transverse temperature gradient
on the relative speed profile.
Sh.Yu.V.
Translator's notet This is the full translation of the original Russian
abstract.
Card 3/3

USTI I B. P., an(JA Vulli-a-, -1. -r.)
"on the Aerodynamics of the Cyclonic Furnace Chamber.." Aerodynamic and Heat
Transfer Problems in Boiler and Furnace Procesees; A Collection of Artf-cles,
Moscow, Gosenergoizdat, Moscow, 1958. 329 p.
Purpose: The book is intended for engineers and combustion specialists concerned
with the design and operation of heating equipment and it is also for scientific
workers and students of vtuzes.

Savesh:h.,,I.ye In prilaadr..y C-ovay dir=ikc. 1956
Trudy Scveshchaniya To priklails*Y EMZDVOY C. AL--X-a, 23-26 zity-br.-
V.3% e. (Tmnc&ctIarx. of th~ ConfLmncc on Applied Gai by.4=icj, B,~!d in
Al--AtA, 2)-:6 October *56) Alra-Ata, I=d-vo Air X.zzal-lak~y S'~It, 15,59.
255 P, Errata allp Lmerted. 900 copies rrirteA.
Spomoring Aqgency: Akslcmlya nauk KmzakhsVoy SM. V---Wiskily so.-udA=trcrryy
univerattet Scent S.M. Kirova. -
Editorial bold. Bear. Ed.% L.A. VulLs; V.P. Kmhkarvv; T.P. L~Vye~ and
D.P. Ustivenko. Ed.: V.V. A1ckz=dxIys'x1y. Tech. Ed.: Z.P. Rom"ta.
PMUME: This book In lnte~~&,d for perzonnel, of scientific research 1.~-Itutco
and Jrlustrial erZIncers in thc field or applied fluil ~chanics, &-,I
be of Interest to students of advanced courses In the field.
Transactions of the Conference (Cont.) -/5zw
CWUL&GE: The book consists of th~ transcriptions or 31 psem read at the
confemr-ze an zAa dy~&=Ica which was convvned unler the initiati" of the
K"akhkly govud&r*t%-cAnyy ur~ivcraltct 4wnl S.M. Kjro,, (xamkh State Unl%~r-
alty Iw&I S.M. Kirov) and the Inatitut encrLet1ki Ak~%--4i rAuk
SSR Institute of Power EUineertng or Ox AcalcrV or :,clences Kazuk_,uk"
W11) and held October 23-25, 1956. Three br~hca of gas k-,des
wm djacusseds osrs~ly-. jet flow of, lie
.uids &nS gmsess aerodynamics of
Peo~c-scs. and the Outflow Of liquids. The practical of the
~Transactioneof the confemme consiats in the adaptatio,
.. of cheo-y to
wth-'>d' Of tccb-lcol cOrlutmtiOn and Oaft3urlne vethais related to
fumaces, and ott~,r Industrial p~c44- in which V~wocn--A play
a Pmdomlvart rulA. Eight papers real at the Confem=c are not 1_~~Iwlcl
In Wa collection for variou. reasons. Tbe "thom of the d.slrZ palem
arot L.D. W~ (Tbc~l and AcrodyrjL=ic Chft~teri.tiza of Pulwrizel -.a
rlace DArners) and A.A. Goleyevakly (outlincs -1 Physical M,,dcls of the J,t
XDtlOv H&cbwlcs of Fluids), W.I. Akatnov, Yr. P. Boelan&v, S.V. Bukh~,
T.K. Kironecko, &.a. nazryo~, and G.V. Ya3wNrv. L.G. Loyts~anskly is
wntloi~d " being in thtrge of s, deWtennt of thr Katayh State Craw"Ity,
and I-V- Wrlk~j Candll,~t& Of MY34cal and HatherAtIcal Sjencea,
a cember of the sane ~Ivemity. neferonces am fo~,I a- tb- coj at
Session or 0-tober 24, 1,W
C.S. 1~4tiCatina Turbuj~pc-z Ch~actcrt*tjcs Or a
Fr- ftnisotheMic Jet am an 0ien FI&- 65
Y~zhl~, V.P. (C-did.t~ of ph:,.Ic&l and K,...
__tLc.1 Sole".47.
Cr- Pa"11cl ~4 CO.--tmrY 1"tin' or I'- Unifl- Fl-, of C~;rcazible G~ 55
Tm"a-tim, of the Conr~mr- (Cont.)
Lcontlyc~, T.?. of I chnLcal 1~!ercra), ~p-44on Of
A.xially Byricotrics.1 J~ts Sr. FamIUI -A Contmry Plo-
NWI~, S.V. ReL!UIA-Ity or Moto, "a C--hu3-1., of C"'I Prtlcl-
gaz-amhuk, X.R., and r.T. Pol'skly. On th~ Crtils In f~, VI-cus
r1- of Gas In a Plare P.mll,l Chanrl C.)
C.nt,~ts of the Discussion In TI.-L,f
ScasLOn of Octotvr 24, I-Y~(
T~mkhlna. r..r. Far-sicn or an Axially Sq---trickj J~t of O~ In a
W,Ilun of Djffcmr-. :kmzity
Cbwbysh-, r.v. Y cl,ktrat, Uj tch-ILly irstttj* (AII-17-11~
Flect-tech,I-I 1-titut')), a,! V--r
U., In C- Flow.
C.rd 5/)

Trura,etiona of th~ Corrcr-= (Colt.) we/5--n
?rorimr.,~, A~T. Jrva~tICmtlrZ a ',rrdmttrlcte-I TurUlefit Jet m
Akat~, N.r. Zurway or th.- Works of tbe Dopartwrt at HyIm-.-ro-
d~i4tlcs or the Lcr.!rr;rmd iolytoctnleml 1.~tlut, i.-M. YAUMn
or. the Jet Thcor7 IM
Sbcj-lc~, S.F., sni S. Tsay. P1we Jet ir . Cra- %~tlon of an
Xtr Conduit i0q.
besjvao~, V.G. Use of MrAmIntri:rmtors F~r SolvirZ Jet Pmb%e~
Contcntz of tt,- Mecusaim in Brief
Session of October 25, 1956 (MOmXnc:)
Utzml -son, D.D. JCamdld%tr of Teth.,le&I Sciences; Docent; Tsentrul Inyy
kotlaturbimyy institut lWrl Pol-mova, lentrerad (Central Turbire ard
botler Inatitute in~rl Pol-unov, 1,eninprnA)I.
Sainr Proble~4 of the AeroIy.-,=tzs of Furnazo Cyclorr Charl-ro w64 of th~
Co4=tibn of Coal Powder FUlverized Coal 125
C.rd Ch
7r%ns=tlor, n' the Covfamrre (Cart.)
rstleer,Wo It P Candlda.e of Tecbrlml ~~ttrrc~j, of
4;4;k~~e: " or a Cyclone Ckv-.~,,r 131.
Volkov, Ye. V. Son.- Acml~,rnmjc or . r,,o-n-, Flow in
& Cyclone Furawe U-1
Tor-%omciys A.T_ m,-A I.P. Lasim. Or. the Problem of the Worklrg
Process In a Cyclme Cl,=bcr 252
Takabov, O.V. Genermlitire krodynamic law3 of Cyclo~ Ch&mk*rs 10
Contents of the Discuaslor. in Brief 10
Session of October 25, iq% (rvvrtrz)
Re,pYaVov, 1-2. (Doctor of' Tcchxicall IntUtut emri:~tjkl
(trstit.t, of' Power EaCl-erlre)j. U.11~1- TU- or haverimel Coal 163
Tel~ci-, A.S. IteCultritles ..' C- ra,- Burr.Ltg V Z,
Card T/9
Tranz4ctt~z of the Confemrce. (Cbrt.)
Y.rshl., Sh. A. Acrady~,,ic, of , Tubule~t c,, ri,~
rlokArev, ?;.r. (C~IlUte of T-N!L-Ol lele,.~~x; Umllakty
las'Itut I-i Ximen, (U.-.11
Polyt-h~ics`l lr-%Litu'~ 1-1 Mmv, Irt-trIal
T-dtlrz or -- C~ H'.t. of Or- Ff-rth RA.-O
r,ICd-rxrI, Y.. F. 0. th, lt~?
or tk, G~jftc-jrn Preeen,
C6ntcr.ts of' %14 Msmm~im Ir Brief
Firml October 'N,
rump I Of we.' rio- t,~ tro- 1-titut Trere, tIkl
AN (1--tute of F'o-, r
::.V. r-te rr~tl-- or Fi-
l'ourz". cordi-J.-
C,rl V~

10(2) PHASE I BOCK FXPLADITATICIN SOV/22TI
SOT&AbchltnlYo po prikladnay gazovoy dimalk*. Aim&-At&, 1956

Trudy (Transactlc-~s of the Conference on Applied On's Dynamics) Alm
Ata, Izd-vo AN Kazalchzkoy MR, 1959. 235 P. Irrats allp Inserted.
qfv~ , ' - - - , ,
Sponsoring Agencys Kazakhakil gosudaratwonnyy unlveroitot Imeal B.N.
x1rova,
. Rorokinal IdItortal Board
Id.s V.V. Alskmandriyok Tech. Id.s Z
!
Tr. loontlyeve. and M.P.
;
L.A. Yulls ( Reap. X gashkaro
Ustimako.

nR?CSZt This book should bs of interest to scientists and oftalneers
working an problems of applied gas dynamics and my be of use to
students.
COVERAGXi This book presents reports end brief summaries of the diA-
cumalons which took place at the Conference On Applied Gas Dynamics
In Alma-Ata In October 1956. The conference was oubdIvIded Into three
areas of applied gas dynaulcat jet flows of fluids and gowns, the
'~,~r~;dyna~!cs of heating processes, &n-3 the dischar of & fluid
C
nearanoci*
Th. practical value of the "TransActlooD of the Co
consists In the development of theory. movio" or technical cal.
culation and methods for x7atematIc "aaurement applied to hoot.
In&, furnace, and other "uatr!Al pr*oaaaoa for wh!.ch, in most
cases. Aerodynamic phenomena are docirIce factors.
--
-
_
t_ii;;Ory by t~o Chair
lkatrov-P.I. Survey of Articles
an is
of Hydro- and Aerodynamic* of the Leningrad Polytechnical Institute
ljwnl M.1. Kalinin 107
Sh*peloj, Sff-, and S. Tsoy. Two-dimensional Jot in the Croso
Section Of an Air DudT- 108
Boopalova_JL2~ Una of Hydrodynamic Calculating Nachinea for
th-e-So'lutlon of Jet Problems 115
Brief Summary of the Dlocuselamns 122
Session of October 25, 19% (morning)
KaUpellson 13,D Some Problems In the kerodynamiles of Cyft.
Com;Uil~~&;;rs and the Ccobustion of Coal Dust 123
A;ax1awWL9__L.Z. Aerodynamics of Twisted Jet* and Cyalass
Chommors 134

VULIS, L.A.. prof.. doktor takhn.nauk, otv.red.; KASU"V, V.P., kand.
fiziko-metemat.nauk, red.; LIONTITIVA, T.F.. kand.takhn..nauk,
red.; JPT 0, B.P., kand.takhn.nauk, red.; AT:IZ*.qA_VMrrSM,
V.V,, red-,-,- R(IROKM,-'--Z.P., tekhn.red.
LFroceedings of the Conference on Applied Gas Dynamics] Trudy
Soveshohanlia po prikladnol gazovoi dinamike. Alma-Ata, Izd-vo
Akad.nau 4s=. 1959. 233 P. (MIRA 12:6)
1. Soveshchaniye po priklednoy gazovoy dinamike. Alma-Ata. 1956.
2. Lasakhokly gosudarstvannyy universitat im. Kirava; Institut
energetiki AN KasMM, GAlma-Ata (for Vulis).
(Aerodynamics)

TUTIS, I.jl.; U'Kll,:;IZO, 3.i~.
Calc-.ulatini~ heqt trnnsfer to lic,ild nritpl.-3. 1-7,. AiT *,, CZ
__n r_-. , -R.
Scr. erior.~-. 159.
(Haat trAnsmioslon) (Lioluld metals)

USTRENKO, B. P..) BESPALOVA, V. G., VULIS) L. A. (Alina-Ata)
"Liquid-Flow Analogy in the Treatment of Problems Concernin;; the
Propagation of Turbulent Jets."
report presented at the First All-Union Congress on Theoretical and Applied
Mechanics, Moscow, 27 Jan - 3 Feb 196o.

ARTrM, L.; VULIS, L.A.; USTIMBW# B.P.
Hydrodynamic tbeory of beat transfer applied to
liquids with small Prandtl numberse Izv.AN Xazakh.
SSR Ser.onerg. no.2:76-89 160. WRL 13:7)
(%rdrodynamics) (Heat--Tranomission)

28373
A001/AIOI
AUTHOR: Ustimenko,.- ~.P.
TITLE: Investigation of plane turbulent Jets with a complicated initial
profile of velocities
PERIODICAL: Referativnyy zhurnal. Mekhanika, no, 8, 1961, 3_3-34, abstract 8B208
("Izv. AN KazSSR. Ser. energ.", 1960, no. 2 (18), 68-83, KazaYh.
summary)
TEXT: The author describes the results of an experimental and theoretical
investigation of: 1) a plane turbulent jet outflowing from a nozzle of finite
dimensions, 2) a composite plane jet consisting of two finite parallel jets of
different velocities, and 3) two parallel plane jets at various separations be-
tween them. The theoretical analysis of propagation of plane jets is based on
the using of equation of motion (or heat transfer) of the type of heat conducti-
vity equation. 8olutions of this equation are derived for the types of jet flows
mentioned above. The sketch of an experimental installation and the method of
measurements are desdribedv To obtain a plane jet with uniform distribution of
velocities at outlet, a profiled nozzle with 11-fold compression was applied. The
Card 1/2

2" 373
S/124/61/000/008/'Oi7/042
Invostigation of plane turbulent jets ... AOOI/AlOI
air supplied by a fan could be heated with an electric heater.. During the ex-
periments the magnitudes of dynamical pressure and temperature in jets were mea-
sured. Dynamical pressure was measured with a Pitot tube with inner diameter
0.5 mm. Temperature was measured with a nichrome-ccnstantan thermocouple. The
author presents the measured profiles of relative velccities in different sec-
tions of the jets, which make it possible to judge on the structure of plane Jets
of finite dimensions with a complicated profile of velocities at the outlet. from
the nozzle. He shows the possibility of employing, for calculations of jets, dif-
ferential equations of the type of equation of heat conductivity, if an empirical
formula is used for transfer coefficient. There are 6 references,
Yu. Dityakin
[Abstracter's note: Complete translation]
Card 212

357h8
S11 24/69/'OOG/UO3/()23/052
7-1-1000 D237/D301
//. 3q00
AUTHOR: Ustimenko, B,.P.
TITLE; Heat transfer to liquid metals under the conditions of
the inner problem
PERIODICAL: Referativnyy zhurnalf Meknanilcal no. 3, 19629 93,
abstract 3B583 (Tr. in-ta energ. AN KazSSR, 1960,
t3
252 - 260)
TEXT: Utilizing the facG that for low Prandtl P.1c's characTeristic
for liouid metal heat transfer media the thickness' of z.-,e ihermal
boundary layer exceeds the thickness of the dynamical layer by nany
times, the author simplifies the equations of heat transler in a
circular tube, i.e. he assumes a homogeneous velocity field, ard
neglects longitudinal heat transfer as opposed to the transverse
one. The resulting equation is ounalogous to that of heat conduction
in the rigid, circular, infinite cylinder, whose solution is known.
In this approximate formulation, profiles of relative temperatures,
the len,-th of the section in which heat transfer stabilizes mid va-
lues for the Nusselt No. are obtained. Comparisons are made of the
Oard 1/2

a t
S/124/62/030/003/023/0c/2
Heat transfer to liquid metals ... D237/D301
obtained approximate results, with those obtained by other authors.
[Abstractor's note: Complete translationi.
j-
Card 2/2

USTRENKO,, B. P.7 BARLYBAYEV, K. A., BUKMW4, S. V., and ZRUBGEnAYEV, K. A.
"Some Problems of Heat Transfer by Convection in an Incomprewilble
Liquid (internal Problem)."
Report submitted for the Conference on Heat and Mass Transfer,
Minsk, BSSR, june 1961.

USTDOW, 13. P.) VMISI L. A.) LEONT'YEVA) T. P., PALATNIK, 1. B., and
SAKEOV) Z. B.
"Thermal Problems of a Free (stream) Turbulent Boundary Layer."
Report submitted for the Conference on Heat and Mass Transfer,
Minsk, BSSR, Ame 1961.

USTDZNKO, B. P., ZHURGENBAYEV, K. A., BUKHKAN, S. V. andBhRLYVAM,, 10i. A.
"Several problems of convective hent-exchange in non-compressed fluid
(internal problem)."
Report presented at the Ist All-Union Conference on Heat- and Mass- Exchange,
Minsk, BSSR, 5-9 June 1961

USTTIENKO B. P.; SAKIPOV, L. B.: PALATNIIK, I.B.; LEOTIEVA) T. F.
I'Thermal Problem of a Free (Jet) Turbulent Boundary Layer"
Report presented at the Conference on heat and Mass Transfer.
Minsk, USSR, 5-10 June 61
General -problem of heat and Mass transfer are discussed and method
of solution of heat and dynamic problems of stream flows is given
in this paper. New experimental data for cold, low-heated flat
and axis-symmetrical streams are presented.

USTIMENKO) B. P.
"Some Problems of heat Transfer by Convection
in an Incompressible Liquid (Internal problem)"
Repor-". -presented a5 the Conference on heat and Mass Transfer.
Minsk) USSR, 5-10 une 61
The results of theoretical calculation and experimental investi-
gations or hydrodynamics and heat transfer at a forced flow of
incompressible liquids in channels are presented in the paper.
Besides the6retical and experimental investigations the given
problem was also solved with the help of the system of the ana-
lytical integrator of the Lukyanov system.

BARLYBAYEVp Kh.A.; BUEMAN, S.V.; ZNUAGEMBAYEV, K.A.; USTDIRIKOp B.P.;
ATENKOVj S.., tokhn. red.
[some aspects of convective heat transfer in an incompresgible
fluid (internal problem); Conference on Heat and Mass Transfer,
Finsk, January 23-27.. 19611 Nekotorye voprosy konvektivnogo
teploobmena v neszhimasmoi zhidkosti (vnutrenniaia zadacha);
soveshchanie po teplo-i massoobmenu, g. Minsk,, 23-27 ianvaria
1961 g. Minsk, 1961. 17 p. (141RA. 15 :2)
(Heat-Convection) (Hydrodynamics)

S/ 1 37/62/G0Q/C()7/0_105/072
A057/A1O1
AU'l-IORS Zmeykov, V. 'N., Ustimenko, B. P.
A
TITLE. investigation of the heat emission to mercury in the transition
range under conditions of the inner problem
PIMODICAL: Referativnyy zhurnal, Metallurgiya, no.'7, 1962, 9, abstract 7149
("Tr. in-ta energ. AN XazSSR", 1961, 3, 147 - 155)
TID.T: The heat emission of technical Fg was investigeted in the transi-
ticn zone from laminar to turbulent movement (300 !~ Re 4.25,000) in cylindrical
tubes of stainlers steel (diameter 1.5 mm, ratio length to diameter 1/d - 100)
and of Cu (diameter 2 rjr,, I/d = 75). The investigation was carried out based on
a mothod which allowed the elimination of the measurement of the temperature drop
bet,acen the inner surface of the heat exchanger and the heat carrier, by a pre-
4.
liminary calibration of the device with water. It was observed that 'he Nussel.
number Nu decreaoes sharply with a decrease of the Pekle number Pe down to values
which are smaller than boundary values for !a.-,Iinar conditions. Such a drop is
explained.by heterogeneity of the heat carriers. The form of the function
Card 1/2

Investigation of the ...
Sl'. 37/6Z/C,00/VD7/U'35/C,72
A057/A1O1
x (.,/ o.-14 (Re) for Fg is analogous to the function for cornion
./ Vw
jiquids. Theie are 11 references.
L. Bystrov
[Abstracter's note: Complete translation]
Card 2/2

LEONTIYEVA, T.P.,- UST.DENKO, B.P.
Studyinr the aerodynamic" o,' i plane flow in a uniform opposing
jet. T#udy Inst.energ.All ldigakh.SSR 3:156-166 161.
(MIRA :L4!12)
(Aerodynamics)

1 1657
B/196/63/0,dO/001/020/033
),V 0 E073/E435
AUTHORS: Ustimenko, B.P., Zhurgembayev, K.A.
TITLZ t of a iiydraulic integrator for calculating
the convective heat exchange under conditions of the
internal problem
PERIODICAL: Referativnyy zhurnal, Elektrotekhnika i energetika,
no.1, 1963, 4, abstract 1 G21. (Izv. AN KazSSR. Ser.
energ. no.1(21), 1962, 95-108, Kaz- summary)
TEXT: -The results are described of work on applying the
....~hydrodynamic integrator for calculating the convective heat
exchange under conditions of the internal-problem. Particular
attention is paid to evolving the theory of the instrument. The
solution Is described of the problem of heat exchange In plane
and circular channels for the case of a constant velocity profile
(W - wcp) and for the case of a laminar flow of the liquid. For.
boundary conditions were taken either qn - cOnst or On = const
where On - t - (t - tn)/(to - tn), t - teniperature of the flow,
tw - wall temperature. The results of calculations on a hydro-
integrator showed good agreement with the.available.analytical
Card 1/2

s/196/63/000/001/020/035
Application of a hydraulicl ... E073/E435
solutions. It is shown 'that for the same tb oundary conditions the
heat exchange intensifies On transition to %kitnore blunt velocity
profile. For a given value of the velocityprofile larger Nu
numbers will be obtained T8r the boundary corldition qn = const.
The results of solutions ~f the problems of'heat exchange in
channels of a complicated~'donfigurationps'ifelI as of the heat
exchange under turbulent flow conditions will be published later
9 references.
[Abstractor's note: Complete translation.]
Card 2/2

USTIMM, B. P.
Research into the Vechanics of Liquids and Cases Conducted by t-e -Lr:erm~)-
N!. v
1,
pbysical Laboratory of KAZAKH SttLte University ir-eni S.
p. 129
TRANSACTIONS OF THE RND REMBLICAN WDEMICE Oil MUNTUMATICS AND MECIV.NIM
(TMW VTOROY RESRM.IKMV')Y WAMEMMI1 PO VAT:~IATTKF I WJW-IME), !R):
pages, publiBhed by the PubliBbing House ol the AS WAM SSR, Mkk-ATA, USSR, 1962

USTI.MKWO, B. P. ; ZHURGDSX!OJ', K. A. : NTLJSUF_PIYOVA, i). A.
"The calculation of convective heat transfer of an incc=pressible 2.iq%if.-_~
complex-configuration channels."
report submitted for 2nd All-Union Conf on Heat & Mass Transfer, Minsk, 4-12
may 1964.
Power Inst, AS KazSSR.

ZEKEKOV, V. N.; USTIMEM, B. P.
"Hydrodynamics and heat transfer of rotating flov between two coazial 2ylinders."
report submitted for 2nd All-Union Corif on Heat & Mass Transfer, Minsk, 14-12
may 64.
Power Inst, AS KazSSR.

ZP4TI~~
ZI,IEYIII~.'C,V,V.N.;~.fft'iN',~',Ii:-)Ci,ill.~A.-,,U-JTI'--'--C? --I Y. (-Al7a-' t )
'; a
. . .L _'; 11. 1 D.
"Hydrodynamics and heat transfer In the annular canal with
an Inner rotatirg cylirder"
report presented at the 2nd All-Union Congress on rheoretical
and Applied Itlechaniesq Moscow, 29 Jan - 5 Feb 64.

VULIS,, L. A. (Leningrad); YJOLE-1.1-21, V. Ye; FAIATNix, 1. B.; SkKIPOV, Z.;
USTD.'-'kIEOj3 P (Alma-Ata)
"Laws of propagation of turbulent conpressibie gas jets"
report presented at the 2nd All-Union Congress on Theoretical and Applied
Mechanics., Moscow., 29 Jan - 5 Feb 1964.

ACCESSION N'p: P 4
AUTHORS: Ibraqmov, B. P,
TITLE: Expe I--,IT)f =i x ~ 3 .13,lirne! ral S err.~ -
bounded )et in m a(
SOURCE: AN Kaz!;SR. IzveStiva. Ser_,ya ~~i,,-l'-o--pater,-.al~ic-lieskikh nauk,
no. 2, 1964, 87--95
TOPIC TAGS: flow kinetics, -ia; let, wall effect
ABSTRACT: The -espar-~- r(--p,-,r* is par, an investliqv-ion of tYe
aerodyniamLcs c_,f sem-: o,,: a- the neat-
~lv F; If, a-ho r a,- va2 sk).y Ln-
777-17-
4~
al,
purpose ~s F ot
Card 1/3

L 17679-65
ACCESSION NR: AP4049400
rod 45 mn in diameter and 1.5 me~:er long by means of a fan, a tur-
bulizer, and an annular sict. Another fan and turbulizer p-roduced
the uniform, accompanying streEtm. The pressure was measured with a.
pitot tube that could be moveo in three -~':_mensions. The stream
velocity ranged frou thp- veloci_t~.,~ from 28.6
to 47.9 m/sec, and their ratio m ranged from. 0 co 0.0,25. Measure-
inents w,2re made -): `*_Z'r'_-":_'_ - ': 1. ,r!~,jient f-1--tior. and of :he
momentum transfer coeffIcier.t. ov-r t~.e ent.re ran(g.2 cL' rr.. ne re -
sults demonstrated the self-sLmilarity of the velocity profiles in
the transverse sections of the Jet and along -he j,-t, for fixed
values of m. It '~S show-. t'~at' Unlike free )ets, an increase in
the parameter M of the wall -:,et. j L is
concluded that further studlv _,S
of zhe stream under thermot~,ramic (-ondlticns and Lhe formulation of
r as
a physically. ~-a!:-~ - t : . . - -
figures, 8 formulas, arid I
Card 2/3

us i
SUBMITTED: 00
SUB CODE: ME
Card 3/3
ENCL: 00
VR REF SOV: 005 OTHER: 003

ACCESSION ITR: AP4039226 S/0031/64/000/004/0063/0089
AUTHORS: Ibragimov, 1. I.;__UatJ-enko,__B,.___P_..
TITLE: Experimental investigations of exisymmetric semi-infinite jet in wake flow
SOURCE: AN KazSSR. Vestnik, no. 4t 1964, 83-89
TOPIC TAGS: jet aerodynamics, pitot probe, concentric nozzle, wake flow, turbulent
jet# friction coefficient, velocity profilet axisymmetrio jet
ABSTRACT: An experimental investigation has been conducted on semi-i.-Xinite jet
aerodynamics in the Thermophysics Laboratories at the Khazakh Scientific Research
Institute of Power Engineering. The study involved the turbulent jet generated
along,cylindrical walls in wake flow. The experimental equipment consisted of two
concentric nozzles with the jet issuing from a circular alit along cylindrical rods
coaxial with the nozzle walls. Profile measurements were made using pitot probes.
The results are represented graphically in terms of excess velocityl , - 'now,
profilesp both transverse and longitudinal in the jet for various parameters
M - Uflow/u jet' Prom two-dimensional hydrodynamic considerations an expression is
derived for the turbulent friction coefficient in the semi-infinite jet for a
. - 1/2
Card

ACCESSION NRi AP4039226
velocity profile given by u/Um where ip Y The results show
that increasing m has the effect of increasing the jet decay rate. Orig. art. h&sg
,8 formulas and 4 figures.
I
ASSOCIATION: Laboratoriya teplofizil:i KazakhOkogo nauchno - isel0dovat*1113kogo
.inatituta energetiki (Thermop sics Laboratory at the Kazakh Scientific Research
;Institute of Power Engineering~
SUBVITTEDs 00 DATE ACQ: O5Jun64 ENCLs 00
SUB CODE: ME NO REF SM 006 OTHERs 003:
Card- 2/2

ACCESSION NRt AP4043406 S/0031/64/000/OC/7/0051/0057
AUTHORS: Nusupbekova, D. A.; Ustimenko, B. P.
VITLE: Calculation of laminar convectional heat exchange in a flat cux-ved
channel
SOURCE: All KazSSR. Vostnik, no. 7, 1.961*, 51-57
TOPIC TAGS- Nuscolt number, heat oxcliango, Reynolds number, channel flow, heat p
transfer coefficient
ABSTRACT: The study of mathematically precise equations for theoretical consider-
ation of laminar convectional heat exchange in variously curved channels explains
the mechanics of the process and requirements for laminar flow. Tha hydrodynamics
and heat exchange of an incomt)rossibl.3 liqtLid in a laminar current were troatod
for different relative heat fluxes in the channel walls. Centrifugal force played
a role in all cases except the limiting one where the curvature R
r2
-Fl- (rl, r2 are the radii of the channel walle) was 10 which in the limiting
condition (a flat, straight channel). The speed distribution for.a constant
Card 1/2

ACCESSION NR: AP4043406
flow with varying curvatures ~ms plotted, and the speed maximum was found to
shift toward the inner channel wall as R increased. The resistance coefficient
(drag) 6 was determined, and its value in the limiting condition R = I agreed
with the usual value for resistance in a straight channel. F was plotted for
various Reynolds numbers and curvatures and vms found to increase with higher It's.
Using the thermoconductivo coefficient, the heat flux at the walls, enormr bal-
ance, average flow value of the temperature excess, and boundary conditions, the
temperature profile and heat transfer coefficients wore calculated. NuEselt
numbers were calculated for the inner and outer walls, using heat transfor coef-
ficients.' In both curved and straivht channels the distribution of the dimension-
less excess temperature was plotted for different values of relative heat fluxes.
With a growth of the relative heat fluxes the temperature extreme shifted to the
wall having the lesser heat flow. R's effect on the temperature profile showed
the temperature extreme shifted toward the inner wall as R increased. The de-
pendence of the Nusselt numbers for straight and curved channels was plottod an
a function of the heat flow and R. and it, was found to be qualitativoly similar
for all R. Orig. art. Mai 4.figuron and 21 oquationn.
ASSOCIATIONs none
SUBMITTED: 00 ENCL: 00
SU13 GODE: MAITD 110 REF SOV: 003 OTHER: 002
Cord 2/11)

ACCESSION NR: AP4038440 5/0294/64/002/002/0250/0259
AUTHORS, sUstimenkqt-j~j,,.P.; Zmeykovj V. Ne
)TITLE: ith an internal
Hydrodynamics of flow in an annular channel w
rotating cylinder
SOURCEs Teplofizika vy*sokikh temperatur, v. 2, no. 2, 1964, 250-259i
!TOPIC TAGS: turbulent'liquid flow, vortex effect, flow through
1 annular channel, Reynolds number, velocity distribution, heat flow.
IABSTRACT: In view of the lack of systematic and reliable data on
!!the structure of vortical streams, and particxilarly their turbulent %
!structure, an investigation was made of the hydrodynamics of a V
,icircular stream of incompressible liquid in a closed amiular channel!
liwith an internal rotating cylinder. The setup consisted of two co-
!axial balanced metallic cylinders producing an annular channel 310
mm o*dej, 212 mm i9det and 400 mm-long. The inside cylinder was ro-
Card

,,ACCESSION NRs AP4038440
relative to the outer cylinder by a motor (2700 � 10 rpm), and
,the outer cylinder was kept at a constant temperature with a water
~Jacket. The measurement procedure is described and data on the
,".velocity'profiles, the static pressure, and the tangential friction
;stress are given in detail for different flow conditions and for a
4 5
i,Reynolds number range 10 Re < 10 . A generalized velocity pro
,,file, which coincides in the near-wall region with the logarithmic
,1profile customarily obtained in flow over flat smooth surfaces, is
erived
"obtained also for this case. Asymptotic formulas are then d
!Ifor the velocity distribution and'for the resistance coefficient;
..'these are valid for large values of the dynamic Reynolds number Re+,
1
',Data on the turbulent midrostructure of the stream and on the heat
ji:flow will be reported in later papers. "The authors are grateful
1!:to Professor L, A. Vulis for a discussion of the results and for val-!
uable advice. Orig.,art. has2 6 figures,.21 formulas, and,l-table.
:c,-rd 2/4

ACCESSION NR: AP4038440
tASSOCIATION: Institut energetiki Akademii nauk KazSBR (Institute of'
Power Engineering# Academy of SciencespKazSSR)
:SUBMITTEDs 27Apr63 DATE ACQ: 09Jun64., ENCLs 01
CODEs. MS. NR REP SOVs 005 OTHERl 006
STM
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JIII AP4'038440
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IBRAGIMOV, I.I.i USTIWEITKO, B,F.
F-pprimental inve3tigation of an wall jct. ir. t.~.a
wake flow. Vest, All Kqzqkh. SSR 20 no.403-89 Ap 164.
(MITRA 17-~~;'~

NUSUPBEROVA, D.A.;- UST1WHO) D.P.
Calculation of laminar convective heat exchange in a fla-. c-,i:nr.'-
linear channol. Vest. All Kazakh. SSR 20 no.7t5l-57 J'I 164.
(141RA M 11)

I ~'I~ I-C ~=F_ i, !MI-t-r A 'A
C C Z S S I ON N RA? t4
p. (Candidate of technical Sciences)
AUTROR: Ustizertkai-i,
TITLE., G-jcUj.atj_4tn of free stranily-vartical turbulent jets'by the
equivalent problett oE the 11e;;t conduction tticory
V
SOU7CE: AN KpzSS1. 'estn K,,,,no. 10, 1964, 69-74
TO-PTC TACS, turbil-it F1,-..7. ~-,jrbulvnt vnrtex flnv, turbulent jet
ABSTPACT: The pr.)nosed me,hr~ for the acrod-viamics of
;~:rep, strongly-vortIcal turbulent *,'(Its is 1),isel on reducing the non-
linear equations )f the fre-e turbulent boundnry layer tn equivalent
heat conduction cluattops. This method permitg an arl-)roximate cal-
c U !at i. o no f th e c)n 1, i T-i - i ou F,er.-. i L in i t ta i ve 1 1 c 1 tv ro f i I e
over tlie entire r!gicin of rc -1 7 n -i stronpiv v,) r t i ca Iu r-
butent jet, inclu Jinp tile V p f I o ws -31 'res-
2'j d
2 ii-gures ana 9 _r r m -a al _Q
Card 1/2

Z / Z PJD:)

R
j
rn a - A :a z-aU
TOPIC annual -j F~ t ~j rj-~ 41 n.
L~!~ r~ W T-A L!
r n
an.raial fl--)v, 3elfsin-~'
-Lac
ABSTRACI: The turbi lf,w if tho ~1-- inn-Al tr
-til,J1.1lig cy-Llidur-R is winf, unKrit-r-Al-I h- ro n o!

L 152276-65
ACCESSION NR: AT5)1166,~,
tamperatures, -ind correlations
t~p ,-i, i,tv -eimnc, wnLq

--- --------
57785-65 -2 /EPR/Z,-,[T (1)/FCS (k)/E',,'G (m) Pd-1/1;r-4/
, ~7
pa- 7p-U-7- 'e-d
ACCEESION NR: AR.5014260 UR/0285/65,'000/005/0014/0014
621.438.001.5
SOURCE: Ref. zh. Turbostroyeniy-,. Otdel'ayy v~pttsk, Abs. 5.49.97
A UTHOR: Zmeykqv, V, N.; Ustimeako P,
TITL;-'-. A study cf_jj~~jcs a--id heat ?xchanpc q~ a circular eha_nrel with an
interrail. rotating cylinder
CITED SOURCE: 9b. Probl. teplof.-narg. i prik-1. teplofiz. Vyp. 1. Alma-Ata, An
KazSSR, 1964, 148-1-12
TOPIC TAGS: cimular channel, Internal 7otating cylindisr, heat exchange, aerodynamics,
gas furbine
TRANS LA TION: Tbe report cites letailef! e3cperimental data ort the velocity and tempera-
wro ny-)filf-a, f-riction and heat traaBfer lij a circular charmol with an intern2l
n rtiq: r0,,!Yif4 the friction factor find vei -)city
n
employing tl~e t r I
Card 1/2

L 37785-65
ACCESSYON NR: AR57014260
tfsl d3ta, The 4xpe-r.,menW work w,"s carried out on a gtand
0 40f) mm and an internal rotatiag
M.
ind(Ir with 212 mm. T he r,-q i m
h-f~ te r. vi hil e the exte rna~ 3c(-~
rf '.T).,In.
SLB CODE: PR, TD FNCL., 00
F
'XI
2A
Cord

52275-65
Pd - 1, ~"r -4/ Ps -4/
ACCESSION NR: AT5011667 UPJ3149/641/000/001/0148/0172
AUTHOR: _Zmeyk-ov, V. F. Us t fmenko
P-5
SOTMCFt Alma-Ata, KAT-akhtikiv r-4ri-hn-1 lgled-vptel 'ckiy j1ettt--'Lt j~nerltt
TOPIC TAGS: au-n-u-1ar. (haniiel flow. ~x anni;)ar flryw, annflar f Irra il~ro--ivn'~Mtcs'
annuity,- 11~,w heat c).i;i,ange
-ABSTRAM In spite al" numerous artt-lci on vortex fl.ris (see, e.g., I. S. Biork-
lund, W1. M. Kaus, Trans. ASHE, Serici C, v. 8i, no. 3, 1959; S. 1. Kostertn, Yu. P.
4 - - -)'i'.'T' a
Finat yev, 1nzhe-nF'7T-0 -'4
exchange proper- tes -D 6 -.is a 7 c* nk-m-.M
I F 5 1 A.'.b a r !ia e n- -n
3 t a' ~,na r
12

1, 52275-65
'50115-67
ACCESSION M KI
[Food vIth tirw newly-cfe:welaoEd tauations. Experimental temperature pro -
~A K,, r r I r ia P n r. I I y f,- 1 )~';ed the theore tfcal curver, given by
vartoliii a,itricrs ;Fuj,~ a i
'n '-pI,,)per-dachA, 1962, no.
SUf CODF: twZ TID

ar. t
I . . , I
P,
WRA 2.80)

- ---------
r ACC NRi AT6ool358 SOURCE CODE: UR/0000/65/000/000/0116/0130
AUTHOR: Ustimenko, B. P.;.Zhurgembayev, K. A.; Husupbekova, D. A.
ORG: Instituteof power engineering, AN KazSSR (Institut energetiki, AN Kaz=~_",
TITLE: Calculation of the convective beat transfer of an incompressible liquid in
intricate-shaped channels ~1-1-1-~I,- 7--
SOURCE: Teplo- i massoperenos. t. 1: Konvektivnyy teploobmen v odnorodnoy srede (H
and mass transfer. v. 1: Convective heat exchange in a homogeneous medium). Minsk,
Nauka i tekhnika, 1965, 116-130
TOPIC TAGS: heat transfer, turbulent heat transfer, convective heat transfer, ther-
modynamics
ABSTRACT: Results are presented of the calculations of the resistance and heat tran-s-
fer in the laminar flow of an incompressible viscous liquid in plane rectilinear and
curvilinear channels for various ratior, of the heat fluxes on the channel wal1g.
Approximate calculations-are also given for turbulent convective heat transfer *in
channels using a hydrodynamic integrator. The results indicate that as the ratio of
the beat fluxes on the valls increases, the maximum of the temperature profile shifts
toward the wall having the smaller heat flux. In the case of the laminar circular
flow, the dimensionless temperature maximum shifts toward the side of the interior
wall an the curvature' parameter m increases. Formulas for calculating the Nusselt num-

- - --------
ATbOU1350
ber are given and curves shoving the caq)arative results of the experimental and
theoretical heat transfer calculations are also presented. These results compared
quite favorably and thus confirm that a bydrointegrator may be used to compute tur-
bulent convective heat trbmsfer in various intricate-shaped channels. (TN]
StM CODE: 20/ SUBM DATE: 31Aug65/ ORIG REF., 002/ OTH REF: 005/ ATD PFMS:
Card.

L 11861-66 WrMA WW/68
ACC NRt AT6001361 SOURC.E Ct,,!)E:-. UR/0000/65/000/000/0148/0163
AUTHOR:
kovg V., No,, Ustimenko Be P.
Zmey
~;;?ezS_)SR (I
ORG: Energetics Research lnati+114-el Nauchnc-issledovatelfskiy~
institut energetiki, AN KazSSR)
I
blow between
TITLE: Hydrodynamics and beat trensfor for a twistecf
coaxial cylinders
SOURCE: Teplo- I massopirenose to lt Nonvekti"yy toploobman v
odnorodnoy arede (Heat and mass transfars v, I: Convective heat exchange
In an homogeneous medium)o Hinakp Natika. I tekbn1ka, 1965, 148-163
TOPIC TAGS&O b7drodynamicap convectivo beat transfer,, fluld flowj,
Nueselt number
ABSTRAM The article presents the rosults of an Inveatigation of
hydrodynamics and beat transfer in on annular channel wit'll an inner
rotating cylinders It gives detailed experimental datit on the distri-
bution of the velocity,, temperature,, and pulsation characteristics of
the flows It proposes a scheme for calculation of heal; transfer,, based
on application of hydrodynamic theory and new formulas describing the
velocity profile and the resistance coefficient& The experimental

L 11861-66
__;~Cc
NR, AT6001361
apparatus consisted of two carefully balanced coaxial metal cylinders,,
the inner one of which was set into roteti(3n by a direct cur,,ent method.
The angular velocity could be regulated by a rheostat up to 283 radians/
see, with an accuracy of + I radion/aeo. The channel formed was 0.4.
meters lone and 0.0049 Irrthickness and the diameter of the inner cylln-
der was 0o212 meters* A table shows detailed operating conditions for
all the experiments. Based on this experimental resultes s.figure shows
the universal profile of the d1mensionlese velocity# and a further curve
exhibits the Husselt number as a function of the modified Taylor number.
The article proceeds to an analysis of the turbulent structure of the
flow In the annular channol w1t-h
curve shows the distribution of the pulsation rate," Orige aLrt. has;
19 formulass 5 figures,, and 3 tablese
SUB CODE: 20/ SUBM DATEt 31Aug,55/ ()BIG-REP: nO5/ OTH REF: 009

L J953Z-66 EWT (1) 1 EWP (m) 4w(m) I n~-!Y01b
,ACC'Nlj AT6006926 JWD/WE/GS SOURCE CODE: UR/000O/65/000/00O/GY7-:,-,__
AUTHOR: Karelin, V. Ye.; Palatnik, 1. R.; Untimenko, B. P.
ORG: Power Engineering,Xnatitute, AN KazSSR (Intaftut energetiky AN KazssR)
1,5--
TITLE: Study of heat and momentum trannfer processes in a compressible turbulent Jet
in a cocurrent uniform flow
SOURCE: Teplo- I massoperenos. t. 11: Teplo- I massoperenos pri vzaimodeyetvil tel a
potokami zhidkostey I gazov (Heat ind mass transfer. v. 2: Heat and mass transfer In
the interaction of bodies with liquid and gas flows). Minsk, Nauka I tekhnika, 1965,
399-406
TOPIC TAGS: beat tran r, jet,combustion
!08 -
f-"5- 21114+1 IV
ABSTRACT: The aerodynamids-and heat transfer in nonisotheT
#,pcurrent jets are
I
important for the intensification of conbustion grocesses. comprehensive program
to study this problem was conducted at the Kazakh Scientific Power Engineering Inst~-
tute in 1962-1963. The experiments were carried out in a wind tunnel witli-a test
section 0.6 m in diameter. The jet was preheated by passage through aWWustion
chamber in which butane-propane was burned. The jet was then injected into the test
section through a nozzle 0.05 m in diameter. The velocity of the cocurrent air stres
in the test section was varied between 10 and 20 m/sec to obtain ratios of the

L 2048-M WMIEWP(M)IT-21MM WW/JXT(CZ)
.ACC NR: AT6006423 SOURCE CODE; UR/3149/65/000/002/0165/0172
AUTHOR- lbragmov, 1. 1.; Ustimenko, D. P.
ORG: None
TITLE: Investigation -of the aerodynamics of a rotational jet along a cylindrical wall In a
secondary flow
SOURCE: Alma-Ata. Kazakhskty nauchno-issledovatellskiy Institut energettki. Problemy
toploenergettki I prikladnoy teplofiziki, no. 2, 1965, 165-172
TOPIC TAGS: secondary flow, fluid flav, flow analysis, rotational. flow, nozzle flow
ABSTRACT- The authors present results of an experimental investAgation of the aerg=
dvnamics of a turbulent rotational jet flowing along a cylindrical wall In a se dary flow.
This work Is aTart of the aerodynamic investigations of a semi-boitndary laye flow con-
7,t,,.ducted at Thermal Physics Laboratory, Kazakh Scientific-Research Institute of Power
'Enginceringslaboratoriya teplofizlki K~i_a`RRE_ikogo nauchno-issleLlovatellskogo Instituta
energetiki). The data obtained are compared with data for nonrotational jets. The jets
were studied at different values of the parameters m and n (0 -C- m ~