SCIENTIFIC ABSTRACT VULIKHMAN, M.A. - VULIS, L.A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001961310012-7
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: September 1, 2001
• Sequence Number: 12
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

14.&4-4aty. red.; GLIEW, S.A., doktor khim. nauk, prof4pred.;
GEM?, K.P., ate.mauchn. sotr., red.; GRYWIER, V.S.,
doktor teklm. nauk, red.; DANILOV, S.N., red.;
YEVTUSH121KO, V.A.p kand. khJ.m. naukp red.; ZINOVA, A.D.,
kand. biol. nauk, red.; KIZVVETTEH, I.V.) doktor tekhn.
nauk, red.; KIREYEVA, M.S., kand. biol. nauk, red.;
~VULIKHKAX~.Hp*~., red.; POTEKHIN, L.P.,, red.
(Transactions of the First All-Union Conference of Workers
in the Algal Industry of the U.S.S.R.] Trudy Pervogo Vse-
saiuznogo nauchno-tekhnicheskogo Bove.shchaniia po vodo-
roslevotproagrahlennosti SSSR. Arkhangellsk, Arkhangellskoe
knizhnoe izd-vo. Vol.le 1962. 234 p. (MIRA 17:12)
1. Vsesoyuznoye soveshchaniye rabctnikov vodoro3levoy pro-
uWshlemosti SSSR. 1st. 2. Chlen-lorrespondent All SSSR (for
Danilov). 3. Vsesoyuznyy nauchnyy institut morokogo rybnogo
kho2yaystva i okeanografii (for Kireyeva). 4. Nachallnik
Upravleniya rybncry prornyshlennostJ Arkhangellskogo Bovnar-
khoza (for TSapko). 5. Saratovskiy gosudaratvermyy universiteta
im. N.G.Gherrqshevskogo (for Gl1knan).

VULIKHMAN,, V.Aj FRIDMAN, M.S.; FINKEL', A.I.; YUSIM, G.M.
Autozated production line for low-module wetting of raw materials.
Gidroliz. i lesokhim. prom. 17 no.6t26-27 164. (MIRA 17:12)
1. Ukrgiprogidroliz.

VULIKHMAN.Y.A.1 FIRE]"Olp A.I.; MrWo M.S.
AVtomatle contral system for continucus neutralization. Avt.
I prib. no.4221-22 O-D 164 (MIRA 18t2)

Vumrdw~ V.A.
of the disiolving of &alto Avtom. i prib,
no.4tl3-14 0-4 163. (KIRA l6sl2)
1. Odeaskiy institut "Giproprora."

VULIKHMAN, V.A.; LANTSMLN, P.A.
Automatic line for the production of food salt tablets with macrol.-
and inicro-additives.. Kharch.prom. rm .4sl3-15 O-D 163. (MIRA 171l)

VULIKHMAN, V*A*, inzh.; MOLODETSKAYA, O.T., Lizh.
Automatic control of tank filling arul pump interlocking.
Mekh. i avtom. proizv. 17 no.8-.15-17 Ag ~63- (MIRA 16:10)

--VULIKWAN V.A. lnzh. (Odem); SRTEYNMGj.?.L.p nah. (Odesea)-
Aubomatii~-.Unes for the preparation cf concentratod dry food
for infa.nt feeding. Ilhar.prom. no.21ll..13 Ap-Je 162,
(MA AW91
1. Gosudarstvenny7 institut po proyeltirovaniyu proiWahlenArM
predpriyatiy. (Food, Opneentrateo) (Lasembly-line meth94)

TULIS, A.A.; TERWHIMA, N.N.; CIUMOV, A.P.
WOW .
laws of the propagation of compressible I'lows. Test.0 Kas&kh.SSR 10 no.9:
76-91 5 153. OWU 6:11)
(Aarodynamiall) (asset, flow of)

VULIS, A.L,,,, Inzh.
Modernizaticn - of th---- 7`2-, rewte c-,ntrol imid si,-al-ng dr.;71ce.
,I
Trudy VNIP. no.17:99-120 163. (MIl.'. 17:;9)

AC.' NRi AP6035701 Al /V SOURCE CODE i
MMTORS3 Mityushkinj K, 0*1 Vulisj A. L.; Borisov, G., M,
,ORO: none
h-
TITLE: A remote-control device for a remote signal. system. Class 211 No, 186543
Cannounced by All-Union Scientific Research Institute of Power Engineering and by t a
Plant "Eloktropullt"_JVsesoyuztkyy nauchno-issledovi.tallskiy institut onorgetiki i
zavod "Elektropull t"2/
SOURCE: Izobreteniya, promyshlennyyo obraztsyl tovarnyye znakij not l'?) 19661 147
TOPIC TAGS: pulse signal, remote con~trolj remote control system
ABSTRACT: This Author Gerti-ficate presents a remote-control device for a remote
signal system. The device includes line subassemb31os, selection unituj distributors
with magnetic cores (which have windings superimposed on the4, and output devices.
The design provides for accomplishing the operation of the output devices directly
.from the distributor pulses. The magnetic cores ir;,the device are made, for
,example, of cold-rolled electrochemical steel (see Fig. 1). The output windings of
the distributors are connected'through diode-capacitor circuits with the input of the
output devices. To increase the reliability of the device, the selection units are
made on the bases of a choke circuits The selection units are connected in series
to the triggering circuit and to the releasing circuit of the output devices*
621,398
Card 1/2 T= t

4

ITpi 9
INKRA Ov. V.; VULIS, D.
Now comprehensiva manual on automobile highways. Ayt.tranap.32 no.4.,
39-40 Ap 154. MMA 7,6)
177-~t (Road construction)

VULTS. D.. inzh.
*-----""V'r*a"?:efd-e&paclty of suburban highwa7R. Avt.dor. 21 n0,9:19-22
s 158. (WILL 11:11)
(Traffic ongineering) (Roado-Design)

VULIS, D., inzh,
"Roads on sandy soils* by S.A. Traskinakii. Reviewed by D. Tulin.
Avt.dor. 20 no.ll(l8l)s32-3 of cover 11 157. (KIRA 10:12)
(Roads-Deoign)

VULIS, U.j inzh.
_.-
Some problems in designing highways. A,/t.dor. 24 no.12:22-24
D 161. (KIRA 14:12)
(Roads--Design)

VULIS, D.-A...,.,-inzh.
Byrroads and belt-11-ne highways; technical and econ(mic sub-
stantiation. Avt. dor. 28 no.2:25-26 F 165.
OEM 28:6)

VULIS, D.A.,- Inzh.
Statistical prognoses about automotive traffic patterns. Avt.
dor. 22 no.6:19-?o Je 159. (141RA 12: 9)
(Traffic engineering)

I
f ~_ ~_ -
I _~ /9/~,
Vertical concave curves. Ayt. dor. 21 no.l.*18-20 A 158.(MIRA Iltl)
(Roads--Tables. at,loulations, atej

3/264
/U/000/008/007/008
1064/1242
"AUTITORS:
Vulls, D.A. and Flyakh, VaSo
TITLE: Helicoptori: In road survey
Pr "Y
MIODICAL. RefPrativn-'.1,,' zhurnal,, Vozdushn,.1 transport. 5vodnyy
tome no*Gk, 1962, ~~-32, abstract 6A201. (Automob.
dorogi, no.10, 1961, 3.6-17)
TEXT: helicopters aro utilizod -mainl-.7 in landerpopulqted nnd hrrdly
ac'
cossIble region-c of t1ho USSR, for varioua research projects nnd
particularly for air reconnaissance in"road surveyinge Preliminary
surveys carried out b7 helicopter include gonernl estimate of the
locnl goologicrol and. hydrological conditiofis; * doternination of
competing vAriables of the-gorloral rout~dlraction; Invastigation
'..,J.of the region along mountain rldeea in order to choose the most
suitable saddles and capproache.4 to passes; investigntion of narrow
river valleys and mountain c .anyona In order to decide on route
loen'tions on the one bnWk or the other; Investigation of rivers and
.."I swamps; deciphoring of goologic.al details..in dintricto with pomplicat-
ra'rd .'3./?

S/2t34j6',./00')/006/OX, /0013
1064/1242
lialicopters, In rorid iurvt)y
ed gnnlo(;icPl conditions; aeaiching and aerial reconnaissanco o 'f
urces o qd-bulld;ng votorials; aerial photography end Olectro-
so T rot
11; magnetic and other special technical aerial surveys. The most
conmon hnllcopLers for road. pros pac tlmg are We 1.114 -1 (MI-1); tho
U-14 -4 (MI-4).and the ~j I C24 (Ya K - 24 and the light tvrin-
propeller KAMOV holicoRter,
Abotrootdr's nota:\Cbwplato trnnslation
2/2

VULIS, D,A,. Inxho'ner,
Ok
glectrIc lighting of the automobile hipbvay around Moscow. AVt. dor.
20 no.5:31 My 157. (MLRA 10:8)
(I(oiscow Province--Poadeids Improymment)
(Hoscow Province--Street Iij;hting)

VULIS, D-.A., inzh.,- FIYAYHf V*S*
. ...................... ..... .I
Helicopters in road surveys. Avt. dor. 24 no.10:16-17 0 '6-1-
(MIRA 14:11)
(Roads-Surveying) (Helicopters)

VULIS, I.L.
Statistical estimation of the errors connected with the
linearization of the vorticity equation. Meteor. i gidrol.
no.5:20-27 1,~r 164. (MIRA 17:6)
L Glavnaya geofizicheakaya obvervatoriya imeni A.I.
Voyeykova.

ACCESSION NRz AP40AO30
SM49/6h/000/001/0124/"
AUTHORSs Yudin, X6 I*; Vulis# I*
TITLE: AppUcation of statistical methods to the i6vestigation of the finite
difference structure balance -equation
SOURCI~s AN SM. izv.-Serip goofizichaskaya, no~ is 1964,9 324-135
TOPIG TAGS: statistical metllod.,, finite difference,, structure balance equation;
finite difference equation., spectral denbity,,:error density, arithmatio mean,
geopotential field) wind field
A
ABSTRACT: Starting from some results concerning the theory for the function of a
random variable and from data on the statistical structure of the wind f iWA
and the geopotential field,, the authors have determined the mean arithmetic value
and the spectral density of errors associated with a finito-=ference approxi-
mation of the balance equation, They point out the form of a difference equation
that is distinguished by relatively small error, They conclude that the proposed
method may have comparatively more general significance during analysis of many
natural processes Xor which the atatistical. characteristics of the investigated
Card 1/2

AP403-4030'
ACCESSION NRr
fields are known (structural or correlation functions) arxl which are defined by
equations of mathematical pbpios* Origs arts, hiass 4 f1glires, 3 tabless and 34
4
f or=aas.
ASSOCIVION: Glavnaya Goofitioheskaya observitoriya Im. A. 1. Voyg6va (1Wn
'GeoplWaical'. Obsorvat6ry)
SUB=EDs .23Apr6.3 DATE AcQs' Web64 MOL: 00
-SUB CODE: A~ NO REF SOVt 009 OTIMRs 003
V
Card 2/2

WLIS, I. ; RURGURETS) L. V.; !IJDE.-I, M. I. (Leningrad)
"A statistical approach to the problem of integration of the equa-
tions of atmosphere dynamic"
report presented at the 2nd A3.1-Union Congress on Theoretical and Applied
Mechanics) Moscow; 29 Jan - 5 Feb 196h.

YUDIN,, MOL; ME_I~L.
Use of statistical methods in studying the finite-difference
structure of the balance equation. Dokl. AN SSSR 153 no.5:
1067-1070 -D 163, OURA 1711)
1. G3.avnaya geofizicheakaya observatoriya im. A.I. Voyeykova.
Predstavleno akademikom, A.A. DorodnitsytV

VULIS, I.L.
Stability, study based or,
finite-difference vortex
Trudy GGO no.143:138-3-46
Imitial data of the solution of the
equation for a barotropic model.
t63. (MIRA 17:2)

YUDINP M.I.; VULIS?.j.L....-
Application of statiatical methodn to the study of the finite-
difference structure of the balance equation. Izv. AN SSSR.
Ser. geofis. no.l:'124-135 Ja'64. (MIRA 17t2)

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11.1vor the mi'llikilly hill 14 the
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tial tymnlat.4hou Invou N lit r. With rlqint foruip, r, IS tie-
.re&-. ?, nuoror .1'"I . 6,11--ing
-- whrtr 0.2.1 4 a -; OPA. The ,rtttulti. Are theck,d
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dg4illo Nik"14ey'N fillet. ClArd "it oil
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frACtion Mlul efleff. 4A tuAtcrud C%014"Xe. Nruialli,
anal, 4M. it) Opt efirty. III brat 111.114rr, Iltillor 1 0
V
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.(k -- #)/A: is the "Murlic little qif t
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.11 stir fulletu.1/ta the Initial it's. Re.-Irlortiol. oil
lie Re# iM.-tvill ustucly: f(Hr.1 1; 11
Re.< 1"' 1; Re. >
I'm). r"p. Theme are fitiviijuir irwors, bw cv"Orlpirte CIMI.
14141JIMS. 0,
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Of
09 &--1- ALL 1., 4, p 'U A, I 1-2-m - - - -
N) o
00 4
00
00 j .00
00 41
00
00 100
00
00
00 Velocity of combustion of coal particlivir with st high sob loo
& o .9 content. L. A. Vulis. J. Jerk. PAYs. W-S-43v) Ill. see
00 J ling aIntro. The t-Girt of a
l9fIV%ill9 14Yrf Ulf 4111 On the TRIC Of Ct"111914tioHl 14 Alkli 141- Zee
00 4 60" i% treated 1114themalically all'i laA. are qtcti%-l fi-f 100
the rate tif thickening of the inert coal. For itirvi,
100 a 1.114fKa. And CY11flIffit-41 114M'-11% thil %(1-111 COO
00 "Jay lrj~ $10f only In a 0owing iltnvv3 but, lit I)erijl va"-*.
00 it lit an a"irteration nt the comhustiott. N. Th4m as@
JRAL.jr 400
Moo
Mee
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too
too
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A LL--A WAX 0 Sit 1_ 4
0, to k"Aw" bmew dw mew of WWA b a ON
V' 1. A, CA Aad. &C UMS~ 54
omit k a DAO WOIAMfi~ 10 d0 WOW"C" Of do
09 1 VAs. of l0kh tW S"* 0t 064 Of bft% w " wwk f
dkisilmo(lm (how" omwi.,..Qs as b" 0t *A
srjwkm. a =16 no& of 4
of go-400dw, row% Is 0
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04 moo
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*0
00C1404 AW OWfollti ;ktff
40 A -00
001, 72111 mvmnaw CrT SUPMM41C am= IN GAS FLM. vials, .4141
got L. A. (Rap. Acad, NIN U.S.SAjo .11 be*, 1946, JAj 6696WA-Y. :04
Up to tho prevent, supersonic appoU of gas flow could be obtained 4141
ON only by use or lavallij jet# by uhich transition througb the critical 1410
sound ". 0 is achiewid by successive videning awl narrowing of *00
the channel. It Is slwm that thooratical1y supersonlo appeds 100
60 !1. ;i. of gas flow cAn be otrtainod In other ways (exchange of mass,
i** 0 mehanical ene,ra, or heat).
*0 43 %0
40 - COO
00
"0 0
so it
---r- to=
No&" -00
No is
U 0 of n a it it 1i a No a t FA
;' ; ri
1::U 7* ~Alll
0.0 0 0 9 0 0 Is 0 a 40'41 0 0 0 0 0 0
_0_4
0 kk- io, 0. 0, 0 000,0.0(0 9,9 0 *~'* *,* 0 * 166~"

VMS, L. A.
0 vliianii treniia na per-el-hod cherez skorost' zvuPa. (Akarfamiia '.auk S.'-SR. Dokl,-.~y.
Novaia seriia, 19).,6, v. 54, no. 9. p. 773-775)
Title tr.: Effect of friction on crossiw,, the sonic barrier.
Also published in French in Comptes rendus de 11ficademie des Sciences do VURSS.
Nouvelle serie, 19);6, v. 51t, no, ~, po 769-771 N60-A52)
AS262.0663 v. 511
SO: Aeronautical Sciences and Aviation in the Soviet Union, Librar-
y of Congress, 1955

WWWWWW
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01-10 1 1
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OSM Ceatoroks the Do larowal wook SPW& in
Gas now. (In Ru.M.) L AN . Re He #/ the
YUF 140
Acedtmy of Sciences of V-S
V, $89-672.
Up to the pratent, supersonic speeds of gas flow
could be obtained only by use of Laval's jet, by
which transition through the critical
Is othloved by successive widerting anJ_-U1n11-4:,_n1x
of the channel. It is shown that theoretically su-
personic speeds of got flow can be obtalned In
other ways (exchango, of most, mechanical onenry,
or beat).
a,$L jx1ALxvRrKAL LIMAYWIf CIASSWICATION
L"
10 " V a to at x N&RIF Kan go
60e **0600000000000400*00000*00000*0000000
:1o 0 006000 * 4 0 0 0 0 0 4
Ras
W a 0 9 1 W a All 0
an A* V1 11 'A I
0 0 *000 0 0 0 0 0 0 0 0 0 0 e 0 0 0 0 0
.00
.00
.00
.09
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r**
coo
roe
age
80*
4*0
X99

.4660. IMECHANICS OF FHOPAUAtICU OF DSUMATION AND BURENG. Abramorich,
00 N. and Vulite, Lo-A. (C.R. Acad. SaLo U.R.S.S., 20 Jan* 1947, -410
Vol. 66, (2), 107-110; abstr. in A;jl. Mach. Roy., gar. 1$48, vol.l. -90
A
00 4 95). A study is made of the propag ation or detonation, &seuming that .00
00.1 it consists of a normal shook wave followrod by a burning way*. With so*
004 thIs picture. formulae are derived analo ous to Prand4l's iv*ll-known
h shook-wave relation 1 where VA* = fluid velocity coo
ca, v city. By using the equations of contin- coo
divided by the oriti
09" uity and momentivs far the burning mays which follows immediittely
A, :
behind the shook wave and converts the stream V 0 into stream M.
As authors dorl-re rilatione %hich when analys:i show that the
wavo has ~.he woll-knoan oharacteriatio (usually obtaired
'de tona. ti on
ALAU
-1 by tedious couiputatiOns) that there is a minimum permissible 0
velocity at "Moh Me is unity. It Is noted that the opposite
j extreme the notonatinn-wave velocity is identical with the shock- !bee
wtLve velocit r%*6
# 3r, A farmuls, is derived rolatine the prop"tion
volocity U10- to the thermal cheractortatics of the mixture 01 ire's
_!N- LA 09TAL&UPWAL LITtRAILAt CWSWICATION
too'
-T-*-.TT"TI-W', 4;1-,
U it
0 40 0 0) 0 0 0 0 a 0 0 0 0 0 0 0 9 0 0 a a 0 0 0 0 0 0 0 0 0 0 0 0
-0-00 0 0 6
fil 0 0 a 0 0 0 *-S-A-*-" *-$A

*, 01 4 It V 0 is J4, n , jo b
P Q -K i L
S L tj A I .A - j 1- a, 't-A-1-LAA
0 calibration of the UbbsloWo vircometoro In the envo ol' the Yoske
00 Instrumemt, however, water Is used as the primary stAnds.1-d. 4hU
huonlan nothod for pour point ("setting point") sprearn to be can-
pmrable to that used In G' at Biitain, being defined ati the tempera-
Lure at which tho oil &hovt3 no movement during, one mliiute on being
axnnined In a test tube Inclined at an angle of 450, althovEh the
0,0 deturmf-.atlon or the fncaot figure appears to be a laborious Trocess,
0 o no the oi'f L. heated and re-cooling after every In(31ination of the
tube, which is carrial out at specified temparaturo Irt,.rv%lv. Corrosive
0t "rhur in lubricating olla in determined trf the utual tt?pa of copper
00 test, the rarticuleir choice of time and temrorature in this case being
0 12 hours and 850C respectively. An oxidation test for tranrforzer
oil is laic' down, the: gojernIng condition3 being a duration of 14 hours
at a tenparature of 3.4000 in the presence of both Iron and copper
c%tAlystn and with air blowing. After such oxidation thr, oil is
i-xamlned l'or aludge, acid value, and saponification value. If It is
destred to dotertrins the initial foranation or water-solubln iscide,
thin is carried ott Irl a similAr test, but at 12011C and for a Line
of 6 ~curn. Among the ietlioda Included are some which in Great Britain
are not usually to be ~ f4j~~ ind in
_:w(>rk# bq1nj: r4re In thu
0 'A SL tb91tLLLF-.KAL %1j!*A161j f~41SWOCLY9^0
4% if t. %# N K St a X in tt tr it VA "a it I An A 1 4 N 0 0 0 1 mr 40 1 a 4 1 1
0 9 0 0 9 00 0 0 0 0 4 * 0 0 0 0]; 0 0 49 0 0 0 0 0 a 0 0
0 0 0 0 0 0 0-0 0-0 0
_T_
.00
-00
-00
.00
.00
00
=
to 0
Coe
SO*
-100
400
'too

0 0
0
.
nature uf t( :As cq~- 1,,4 nvt iti c:-;trol. laboi-ittory rather OL-xn on 00

refined by the furfural, nitrobenzoll and phenol processes. The 00
Inclucion. of tests ol this 1ype la rirhipti Ouvv to the fact t1nt ihiareas 00
00 In Vir~ U.K. and U.S.A. their choice is left to the'Individual rofin-3r, the oe
00 at-indard methods of t.eet being intended more to ensure that buyers' *0
00 raq-t.1 rome; vita are detivrmined in a unit'orm r%anner, the State oruration of all 00
00 Induetry In the U.5..';.R. ties made It danirdble that all producara Vrio ftra unitsoo
00 In 4 cingla combine should conforn to a unifort, worki. Control technique. The
i
00 aection (,,n the exhmination"of preAson Ir fairly compr-3honolvo, and in . l
::
00 %driltion to the uruA' I 11hyriesil tofts ouch ar ronctration, drop point, 00
0 0 --tc., Includes ni=broua methods rt%r the chnnical oyAninntioti of greasma, *a
*0 elg., the fletorin-Ination of'fres! fatty acids, soapa, resin. Tests are laid 041
09 down both for evalunt-tig. tho protective action of Creases In rreventing, 00
* 0 corrotJon nivi Rltlo to f.-neuro that the grosses themselves ere free from 0 0
00 corrovive natlon. In the section doaling with ectroluitz. by-products the 00
09 traditional Russian Interest in sulphonic and narlithonic acids Is evivicad b~ 00
of the numerour methods for the eyamination of those materials. Nothods are 00
00 doscrIbcd for the datemination of oil, sulphonic acids, nn,l sulihuric acid 00
we in ffKontnkt," and also :or!evaluating the fat-hylrolyslng activity of this 00
00- material. Products dealt kth in this section Inclule paraffin mx and 00
001 bitument the setting roint'of paraffin wax (often referrei to &a llmaltW, 00
04 point") Is tmkon as the flit protion of the tine-tempersturo cooling CUM6. 00
00 A:V.
-.3 Oil content of rviralfin wnz; in daterm1nvd by a muchnnicnl expression mothoo.0
00 The tests described for bitumen are those usually given in JA-Itiah and Amerl

0

L4141 AtIonsi likewise thitdoscription if sampli" procedure .* conventi
-public
0 0 6 0 0 0 0 0 a 0 0 0 0 015 0.00 9OW -JR 0 0 0 0 0 0 0 0 00 0 0*
0000100046:::9111 04144440d1*4104110100000410OC-0000 1

,i-
-1

this formula Is staid to,rIvs values in error by less thxn two per cent 010
from the more exaot formula, whiah to t4so derived. 00
0 0 0 0 0 0 0 0 0 a 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
IS IS 9 0 a 0 IS a a a 0 0 0 0 0 0 0 0 0 9 0 0 0 0 0 0 0 41 0 0 0 0 6 0 0
00
00
00
00
00
00
0
0 0 0 a

VULIS I L. A.
, .1 . r
I "
0 zakone obrashcheniia vozdeistvii v techenii real Inogo gaza. (APademiip- Rauk SSSR.
Doklady. flovaia seriia, 1947, V. 56, no. 8, P. 799-801)
Title tr.: The law of physical. effects on the character of flow of imperfect g-as.
AS262-S3663 v. 56
SO: Aeronautical Sciences and Aviation Jn the Soviet Union, Library of Congreas, 1955

VULIS, L. A.
Authors VulU, L. A.
Title: Iffia thormodyranica of' gosoouz fl(r4c, (Termodinamika gazwylch yotolcov.) 303 9.
City: Mancow
Publip~erz State Print'ng [louse of Fo4or T,.ngimerlng Litoraturo
Dates 195b
Avallables Library of Congreas
Sounes Monthly List of Hrosian Accessionz, Vol-3 No- 7, Page h59
Call No: QC3IaV&
Suloject: I.. !IhermpdN~nmics. 2. Ono flow,
Imixtb9ok for engineers and students of powerp aeronautical and mechanical engineering iWti-
~~tutions of-higher jearning, The thermodynamic theory of one-dimensional fixed gas flow is
-ical speeds and the formation of shocks.
describea. Special attention is given to crit
Reviewed by G. A. Varshavskiy in Sovetskaya kniga, 1951.. No. 7p P. 35-36.

VMS; L. AO) KUNGERo V. G.;
"Equilibrium Temperature of a Body in GaaeouL Flow$ "Zhurnal Tekhnicheflkol Fiziki
1950, Vol 20, Nr 11 PP 97-109-
"Problem of Calculation and Modeling of Radiating Heat Exchange) Zhurnal Tekhnichesko:
Fiziki, 1954, Vol 24, Nr 11, pp 207Q-2078.- with V- G- KLINGER.
Affiliations: 1. Power Engineering Inst. im G. M. Krzhizbanovskiy. 2. Head of a
Chair., Kazakh State Univ. im S. M. Kirov.

-4:i\
V TJL IS L T T- I i Ei, i
".Iec,ulDrities on the Diatr1uttiun L)-I Gowtorerj6lola zAreaii-1311
Ves'n.
The authors Present an upproximuLo 5c)?u,kjc)n c)f, trie. pro.'I.Cm of the
distribution of a nunl.,~oticler.;i, 1 tUrIOUlellt LLreufa flovilli , out, 0jk'
circular imerture into ~,i flod%led soace. The zol,,Aian is baced on the
assumotion of -llmllaritj 01' volocity-head fiellia. Lxporlrae[AZ wor~~
oerformed to '3iceptain the va.-il(lity of the Lheorotical ra~-ults cai.1; t"rie
aata thus obtained coinc"Ided closely with t'Lie tneorAaticqI pre.'Jictions.
(FZh~'~ekh, No 1, 1U&5)
SO: Sum. 4-92, 12 May 55

W
SGRIPhysics - Gas-D~rna; ics cT FL~:tt Z',-chnn,-e
"Flow of a Viscous G~~s in a Cylindrical Pipe in the Pr-senc~; of Conv--ctiv~~ 11~at
Exchange, 11 6. V. Roj..anonko
DMI SSSHt Vol 91) No 6, pp 14'89-1;.'92 114'3
States that I-i. D. I.Illionshchik and It. K:xistianovich, with V. G. Gailperin and
L. A. 3ironov) on the basis of thi.- classical hydrodynamic th3ory of heat exchance
(see their Frikladnaya Gazovaya Dinamika (AFplied Gas DynaL.ics). 1948 investigated
paidimensional stationary flow of - visc-)us gas in - cylinrlr~cal jApe with
technically sir.ooth walls for the rtave of convective heat exchanCe and const terp Of
the wall. Here the author solves this probleri. under the assurptiona but on the Lasis
of a generalized hydro-1y-namic thtjory of h-at eychanSe that r--fiects the peculi!:-rity of
high-spe,id flow. Cites: L. A. Vilis, To,-,.o-IinnrdJ-a Gazovykh Potik.ov (Therma-lynar-i-dcs
of Gas Flow) 1950- A. A. Gu]ftmn anij N. V. Ilyukhin, 0snovy Ucheniya- 0-
T the ~Scienc- o t
0-MeV pri echanii Gaza s Bol'shoy Skoro3t'yu (Principles of !~ f 113 a
Exchange in High-speed Gas Flow), 1951. Presmterl by Acad 5. A. Khristinnovich
3 Jul 53.
2751'91,

TUIS, L.A.- AVTITY=.qKTT. V.S.. redaktor; SKVCRTSOV, I-it., tekhnicheskiy
ft----IWC*for.
[Thermic combustion process] Teplovoi rexhim gorenila. Moskva, Gols,
energ. lzd-vo, 1954. 287 p. (KLRA 7.'7)
(Host of combuction) (combustion)

VULIS, L.A.
Theoretical calcu.1ation of muffle burners. Izv.AN Xazakh.bM.Ser.
energ, no.4/5:78-89 '54. (KLBA 9: 5)
(Burnors) (Combustion)

VMS, L.A.
Turbulent gas streams. Is-Y.AN Kazakh SSR. Ser.energ.me.6:19-27
1549 (Gat flow) (MLRA 9:4)
Nazakhatani resume:
The author suggests a method of solving the problem of a turbulent free stream of low
velocity flowing into a, submerged space for a significant difference in temperature between
the stream and the surrounding medium. He transforms the equation of the boundary layer
of the stream into new variableso giving it the formof the relativity averaged values of
these new variables. He shows that loss of velocity along the axis of a hot stream is
faster, and of a cold stream slowor than in an incompressible liquid, which agrees qualita-
tively with experience. (IRZhMekh,, No 9, 1955).

TULIS. L#1.; USTIMINKO. B*F*
Aerodynamic diagram of current In a cyclone chamber. Test.AU Xazakb.
SSR 11 no.4:89-97 Ap 134. (KLRA 713)
(Aerodynamics)

VULIS, L.A.; LIMIMA, T.P.; TONKOROGIY, A.V.
Stabilization of a coal-dust torch. Vast. AN X&z&kh.SM U no-5:
34-64 My 134. (JORA ?: 7)
(COMIMstion)
ConWers the question of the possibility- of stabilizing a coal-pulverizing jet with the
aid of countor currents (aarod~m&:Ltc stabilization.) The authors feel that a shortcoming
of the method of stabilization by poorly streamlined bodies ia the fact that the quantity of
raturnab2a hot productv of combtwtion remains constaut. They suggest using a Wagle counter
current whoso speed is greater tfuLn that of the basic liraitless flow. (IahHakh, No 4p 1955)
Sun 606, 5 Aug 55

Category : USSR/Optics - Mysical Optics K-5
'Abs Jour : Ref Zhur - Fizika, No 2., 1957, No 4M
Author vuli L-A-P Klinger, V.G.
- ~ji a ~
Title Concerning the hroblem of the Calculation and Sin-lation of Radiant
Heat Exchange.
Orig Pub Zh. tekhn. fiziki, 1954Y 24, No 11, 2070-2078
Abstract The -equations for the radiant heat exchange between gray bodies, separ-
ated'by a medium that is transparent to rays, are considered. A compu-,
tation procedure is proposed, based on the direct Oonnection between the,
intrinsic and reaultant radiation. The possi'hIji*es of using a ligJat-
ray Analogue of the radiation heat exchange are evaluated.
Card 1/1

('%p 74cr=%atika (llmt P-T Engnq, t", and
At" til- 1, Mp
Ena~hjctcclnlki JWWA95% Y01- 5,--A5-2W)- The aerody-=1
ss
yokne rurm ou-&-roo Vie wvij,~- t~
neo nt~ W
xTbuient i3lilrV. prtw:u In thr Wolone a!.orba- ard Me mat effIcleit Mthed
of i nirc c1 rc cfmw, tiv, n Jr tu(jl,*I. c,'oncrallued ifqutlcn tcl- flon in
oyulane to prQaantaul. (L'i.

PERIODICAL ABSTRACTS
Sub.: USSR/Engineering
AID 4172 - P
-7y ~L. A., and V. P. KASHKAROV.
NII DVUKH ODNORODNYKH POTOKOV VYAZKOY ZHIDKOSTI (On
mixing two homogeneous flows of viscous liquids). Teploenergetika,
no. 2, F 1955: 41-46.
A study on laminary and turbulent flows of twp parallel or
opposite flows of viscous liquids. A mathematical analysis
leads to a formula derived from the analysis of the
asymptotic layer. The velocity and temperature distribution
Is prewented. Five diagrams.

VIJLIS, L.A.; LIONT'YEVA, T.P.
OWN"
Parallel and counter turbulent streams.
no.9:109-122 155. (Gas flow)
Zzv.AN laxakh M.Ser.energ.
Mu 9-5)

A M.-ROMMININAMMMMI NOMMUMM

offiNTIRIPMOF r-Al

VULIS, L.A. daktor tGkhRiVh68kikh Muk, Professorl USUMNED, B.P.,
takhnichafikikh nauk.
Affect Of a noxisothermal field on, the "rody"mics of flow
in & CYClome furnace chamber, Teploanargetika 3 no.406-39
AP '56. MU 9:6)
leInotitut energetiki A6N X&zS*.
(Furnaces-Aerodynamice)
The problem of applying data pertaining to the aero-dynamic properties of a cold air flow
in a c7.clone combustion chamber to the non-Akoothermal notion of a gas flow in the same type
of furnace. Three diagramaj, Seven Russianreferences, 1953-56.

TMIG. L.A., professor, doktor tekhnicheakikh nauk.
1W
Nixing gases by means of jets. Toploonergettka 3 no.12:37-41
D 156. (KM 9:12)
1. lasakhskiy universitst.
(Gas flow)

SOV/124-58-1-833
Translation from: Referativnyy zhurnal, Mekhanika, 1958, Nr 1, p 109 (USSR)
AUTHOR- 4s,-L-A-~- -
TITLE: On the Calculation of Free Turbulent Compress ible-gas Jets (K
Iraschetu svobodnykh turbulentnykh struy szhimayemogo gaza)
PERIODICAL: Izv. AN KazSSR, ser. energet. , 1956, Nr 10, pp 87-102
ABSTRACT: The author presents a method for the approximate calculation of
compressible- gas jet flows; the method is based on the assumption
that turbulent exchange processes in free gas jets are determiniUly
physical quantities such as the density of the flow impulse and excess
heat content but not by the velocity or the excess temperature. This
assumption was verified experimentally by the author (RZhMekh,
1958, Nr 1, abstract 832) for the case of a change in the jet-flow
density due to heating and the presence of gases of different molecu-
lar weight. The results obtained are applied to the solution of the
problem of the starting range of a slightly twisted nonisothermal
turbulent jet in a stationary medium; the paper does not adduce any
experimental verification of the results obtained. Bibliography:
Card 1/1 14 references. 0. V. Yakovlevskiy

Via
SUBJECT USSR / PHYSICS CARD 1 / 2 PA - 1824
AUTHOR VULI8jL.A.t KABICAROVIV.P.
TITLE of a Laminar Vortex Beam of a 11oncompreasible
iquid along the Surface of a Cone.
PERIODICAL trn.teohn.fis,26, faeo.12, 2705-2TO8 (1956)
Issued: 1 1 1957
The laminar flow on an inoomipreasible liquid flowing along a conical surface
is investigatea. An orthogonal system of coordinates is selected in which the
x-axis is located in the direction of the generating line of the cone, the
y-axis is vertical to the former, and the coordinate 9 is read off the axis of
the cone. Zero point is located on the point of the cone. In this system of
coordinates the equations of NAVIER-STOCKS, and those for the untearability of
an axial-symmetric motion is set up for the case that spatial forces are lacking.
These equations are then generalized by means of LAME'S coefficients. On the
assumption that the flow is far from the source , ordinary differential equa-
tions are obtained from which the veljoity profiles (the longitudinal- and ro-
tation components) for the first approximation is obtained for a solution
corresponding to an automodel motion. It would not be difficult to obtain even
higher approximations. Por this purpose it wouldl however, be necessary to do
without the universality of the profiles of the velocity- and pressure-compo,
nents. For the task under discussion here also the solutions of the heat problems
for a noncompressible liquid hold good, which were obtained In a work by
VULIS and TROFIMMO (furn.techn.fin 26, 2709, faso.12, (1956)). The results

Y, I
Zurjf.tsohn.fiepjjjf&~o.12t 2705-2708 (1956) OARD 2 / 2 PA -1824
obtained by:the present work can be used for the approximated representation
of the velocity and the pressure in a turbulent flow at v turb w oonst. The
qualitative character of the motion is without doubt maintained on this
occasions
INSTITUTION: Kazaohian $tata University, Alma-Ata.

J 5)
'SUBJECT USSR / PHYSICS CARD 1 / 2 PA - 1825
AUTHOIR PIJSj A., TRCFIMKO,A.T.
TITLE Beat Problems connected with a Laminar Beam Propagated along a
Wall.
PERIODICAL t4rn.techn.fis,.L6, fasc.12, 2709-2713 (1956)
Issued; I / 1957
The solution of the heat problem for a flat laminar beam of an incompressible
liquid propagated along a wall in found by the integration of differential
equations with corresponding boundary conditions. The two first equations
correspond to the dynamic problem solved by AKANTOV. The problem is investi-
gated for three types of boimdary conaitions: 8T
1. For y-Ol T-Oj for y- oc., TuO, - , 0 (The boundary conditions
ay
for temperature and velocity are similar).
2. For y-O,-2-T - 0, for y - co TwO, LT- - 0 (The beam is propagated along the
ay ay
wall of the non-heat-conductive material).
3- For y-0 T-Tw, for y - oo T - Of !T - 0 (Motion along a wall with constant
ay
temperature). In all thei3e cases T is the excess temperature.
These cases are now dealt with separately. The here obtained results and equa-
tions and final formulae (f,.,)r all three cases) are obtained also in the first
approximation of the heat problem with respect to the laminar beam emitted

V
,Zurn.toohn.fis,26,fase.12, 2'709-2713 (1956) CARD 2 / 2 PA, - 1825
from a radial gap diffusor along a wall. The corresponding dynamic problem has
been solved by CUKKER. The relative temperaturo- and velocity profiles obtained
are shown in form of diagrams. The solution of the dynamic as well as of the
heat problem can be approximatively added to a turbulent motion on the condi-
tion that the coefficients of the turbulence-exchange are assumed to be constant.
The relative velocity profiles according to AKANTOV and the experimental re-
sults obtained by POERTMON differ noticeably. Here the difference in the struc-
ture of "turbulent kinematic viscosity" in a flow near a solid wall as well as
in one that is located at a certain distance from the wall becomes apparent.
The case of a turbulent beam requires special investigation.
INSTITUTION: Kazachian State University, Alma-Ata.

S/123/59/C,00/008/039/043
A004/AO02 -
Translation from: ReferativAyy zhurnal, Mashlnostroveniye, 1959, No. 8, P. 367,
31548
AUTHOR: Vulis. L. A.
C---- I
TITLB% Jet Problems of Applied Gas Dynamics
PERIODICAL: V sb.: Issled. fiz. osnov rabochego protsessa topok I pechey.
Alma-Ata, AN Ka2.SSR, 1957, PP. 15-53
TEXT. The author gives a survey of individual investigation results of
unrestricted turbulent jetslof Incompressible liquids and gases. He Indicates
some problems of -.Nrther invostigations.
Translator's note: This Is the full translation of the original Russian
abstract.
Card 1/1

\/.0 USILA
5(l) 3 PH03 I BOOK EXPLOITATION SOV/1659
Akademiya nauk Kazakhs1coy SSSR., Alma-Ata,
Issledovanlye fiziohealcilboanov raboehego protmesisa topok i pechey
(Investigation of the Bhysical Bases of Operational Processes of
Combustion Chambers and Farnaces) Alma-Ata, Izdat AN Kaz-ikhskoy
SSR, 1957. .369 P, 800 oopies printed,
Additioiial Sponsoring Agency.: Alma-Ata, Kazakhskiy gosudar-stvennyy
universitet. lm. 3.M. Kirov&,
Ed, (Title pgge): L,A,_YUJ1,n., Doctor of Technical Scienceal Profes-
sor; Ed . (Inside lio-o1c); D#X. Glazyrina; Tech. Ed.: ZJ, Rorokina.
PURPOSE: This book is intended for a wide circle of scientists and
industrial engineers,
COVERAGE: The twenty-nine articles of this collection report on
experimental and theoretical investigations of different physical
Card W7

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 ]?rocess applicable to different t3Ties of
burners and furnaces tcyclone combustion chambers, muffle'burners,
burners with automatic stokers, etc.), Artioles in Part I treel;
laminar and turbulent jets of liquids and compressible gas, Part
II reviewit methods of modeling combustion processes (light, hy-
draulic and electrical), enthalpys temperature measurement, oalo-
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..
TABIR OF CONTENTS:
Foreword
From the Editor
Card 2/7
3
5

InvestIgation of the Phyalcal (Cont,) SOV/2659
PART 1. THE AERODYNAMICS OF JET FLOW
Vuliss L.A. w Problems of Gas Dynamioo 15
Kashlcarov,t B,P. Some JkooiWiate.3olutions In the Theory of Inoom-
pressible Liquid Jets 54
Ustimenko,_B.P. The Liventigation of Slightly Involute Jets 64
--Vulis. L.A#" V.P. Kaal.*arov, and T.P* Leo*lyeva, Investiga-
tion Complex Turbulent Jet Flows 86
711~s .1,*Ao, and S.I, Isatayeve Turbulent Plow of an Incompres-
a e quid in the Wake of a Poorly-stream2ined Body 112
Terekhina, N.N. Propagation of a Free Turbulent Gas Jet 125
VuUs, L.A., T.K. Mironenko, and N*N& Terekhina. Approximate
~Mon of Speed and Temperature Distribution in Free
Turbulent Jets of Compressible Gas 148
Card 3/7

Investigation of the Physical (cont.) S"11659
Kashkarows V,P, The question of the F2&t Boundary of a Com-
pr6asible Gas Jet 266
Bukhmsnp S.V.p and A.?. Chernov. The Investigation of Two-
Phase Free Jets 275
PART II* M911HODS OF INVESTIGATION AND PMASURING
_Yulis.. L.A., and V.G. Klinger, investigating Radiant Energy
Exchange-by a Methcmi Mploying Light Models 193
X21nger, V*Q, Experizientsil Investigation of Hadlant Energy
Exchange by an Method EV2oying Light Models. 221
_Yujj~,_L.A,_ The Use of Hydro, Integrators (Hydrodynamic wid
Hydrostatic Integrators] in the Solutions of Some Prac-
tical Problems 223
Potseluyko, V,A,p and A.T. Trofimenko. The Investigation of
a Temperature Fie2d by the X2ectrothermal Analogy Method 242
card 4/7

SOV/1659
:Envestigpttion of the Physical (Cont.)
Vuliso LoA*,p N.D. iosov, and V.A. Potseluyko. Deterudming the
Kemp Constants of Poor Reat,Conduotors 252
'Ydovmnkop Nol.p and V.Vo Favorskiyo The Te4erature Charac-
teristies of Sorae Kazaklistan Coal Ashes 279
Kooovj N,D. 3ome Met~iods of Determining the Diffusion Coef-
ficient of Ganes 285
Kosovp N,D, The Temptrature Dependency of the Diffusion Coef-
ficient of Gases 291
Basina., I,P, Methods of Measuring Flame Temperatu rem in SwbIt-
Ihg Furnaces 297
_W1 i a-L-Aep and N.D. Kosov. A New Method of Calori~etrio
Measurement 311
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Investigation of the Physical (Cont,) SOV/1659
FAJR~ III. COMBUSTION. COMBUSTION CHAMBERS AND FURNACES
Vulis L A Synopsis of the Elementary Theory of Heat Condi-
'~'
--
~~~ng Combustion 321
Favorskiyp V,V. Some bpecial Features of Ash Coal Combustion 345
Rezn~,akovj A,B. The 1haming of a Pulverized-Coal Flame 361
Leontlyeva,v T.P, The Aerodynamios of a Muffle Burner 380
_Vulis, L,A,,, and B.Pe Ustimenko. Investigation of the Aero-
dynamics of a Cyclone Combustion Chamber 389
Tonlcohogiyj A.Vo, and I,P,, Basin&. The Burning and Separation
of Fuel Particles In a Cyclone Combustion Chamber 407
Teplitskiy.. M.G, The Sharp Blast in Combustion Chambers 420
Tonkonogiy, A.V, The Choice of Burners for Reverberatory Cop-
per-Smelting Furnaces 428
card 6/7

investigation of the n7sic4a (C=tq) 3OV/)W59
Tonkonogiy,, A*V*,, and 1,P* Basinae The B=ing of Coal With
a High Content of Mh in a Cyolone Combustion Chamber 447
Favorskiy,, V*V# Some Results of the Study of Working Princi-'
ples of Combustion Chambers With Stoker Orates 457
Suppleisent (From the BdItor) 468
AVAILABIA: Library of Congress
Card 7/7 TWI~b

VULISI L*A.-. USHUROV, V,.P.
#WW,OAI`7- - ,
Slwalating streaml-Laed motion.
i mekh, noo'6:3-3.0 157.
(Hydrodymmics)
P&A 1. IsIr, AN Xazakh, SSR. Ser. mat.
(KIRL 1114)

TULISO L*A,; KASHMOT9 V*~P*
Sim~Uting streamlinad notions. Part 2, Izv, AN Irazakh.- 3SR, Ser;
mat, I mekh. no,'6rll~19 157 (KIU 1114)
~Itrdrodywmlos)

............ ........

VULIS) L. A. and TROMMKO, A. T.
"Heat-Problems for a Iaminar Stream Spreading Along a Wall."
Sov. Phys. - Tecb. Pbjvs. Oct 1957, pp 2616-2620

VULIS, L. A. and KASHMMOV, V. P.
"Psotionof a laminar Twisting Stream df Incompressible Fluid
along the Surface of a Cone." Sov. Phys. - Tech. Phys, Oct 1957, pp 2612-2615.
Derivation of the velocity profile (longitudinal and rotating
components) for first approximation, corresponding to ealf-aimulated motion.

AUTHOR: Vulis, L. A. (Alma-Ata) 24-10-21/26
TITLE: n the Ranque effect. (Ob effekte Ranka)
PERIODICAL: Izvestiya Akademii Nauk SSSR, Otdeleniye Tekhnicheskik-h
Nauk, 1957, No.10, PP.105-107 (USSR)
ABSTRACT: During the flow of air or of any other gar, from a Ranque
tube, a difference is observed in the braking temperature
in the near-axial and in the peripheral streams; the gas
in the tube enters tangentially under pressure and
forms inside it a rotating flow. The difference of the
braking temperature at the axis and near to the walls
reaches several tens of Centigrade. A number of papers
have been devoted to experimental investigation or
theoretical explanation of this phenomenon (Refs. 2,3,6).
For explaining the Ranque effectl the author considers it
advisable to investigate the distribution of the braking
temperature in a steady state unidimensional circular
movement of a viscous gas, for which case the energy
equation can be expressed by means of Eq.(l), p.106. Two
cases are possible, namely, the quasi-hard flow and the
quasi-potential flow. In a real case the circular movement
of the gas is characterised by a variable field of
Card 1/2 temperature bralcing and, correspondingly, by local enerL-y

"Turbulent Transfer of Heat and Matter in a Jet Flow of a Gas," Aerodynamic
and Heat Transfer Problems in Boiler and Furnace Processes; A Collection of
Articles, Moscow, Gosenerg3i.,,.dat, 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 vuzes.
"()n the Aerodynamics of the Cyclonic Furnace Chamber., 11 with Ustimenko, B. P.,
Ibid.

SOV/112-59-20-41797
Translation from: Referativnyy zhurnal. Elektrotekhnika, 1959, 11r 20, p 16,
(USSR)
AUTHOR: Vulis, L.A.
TITLEs The Principles of Gas-Torch Aerodynamics
PERIODICAL: V ab. : Tooriya i praktika szhiganiya gaza. Leningrad Gootoptekhiz-
dat, 1958P pp 5-20
ABSTRACTs The burning of a developed turbulent toich ip considered from the
viewpoint of the theory of turbulent atreamolon the basis of the
asymptotic (infinite) layer theory. A summary of the main charac-
teristics'and solutions for the four simplest problems relating to
free "drowned" streams is given. An analysis of the problem of the
laws of heat and matter transfer in free turbulent streams showed
that t 'he beat agreement with experimental results is achieved when
the.Pr'andtl turbulent number is equal to 0.75. The presence in such
streams of something similar to temperature a,id'corcentration pro-
files can be taken as an established fact. Solutions uf the thermal
(diffusion) problem are given for "drowned" streams* For the indus-
Card 1/2 trial burning of gas the principles 6f turbulent stream propagation
~K

4 7#7>1
soy/112-5n-20-41797
The Principles of Gas-Torch Aerodynamics
in gas currents - parallel, counter and transverse - have a special importance.
The last problem is not solved as yet; for the first two problems solutions are
given and it is pointed out ths,t the method of hydrointegration offers the best
prospects for the solution of equations of the hoat-oonductivity type. It is
pointed out that, unlike the c&se of nonisothermio laminar streams, the calcu-
lation of nonisothermic turbulent streams is based on a hypothesis, subject to
an experimental checks an assumption of the determining role played by the dy-
namic pressure and the density of the current of surplus heat content in zhe tur-
bulent intermixing of gas streams of variable density. Aerodynamic schemes of a
gas torohl essentially diffusional, are considered. The existing methods of cal-
oulation of such a torch are analyzed and the necessity of a further elaboration
is emphasized.
A.D.A.
Card 2/2

22911
S/112/60/000/003/001/002
E073/E335
AUTHOR: Vul"s -L.,A.--
TITLE: Turbulent Heat and Mass Transfer in the Case of
Jet Movement of Gas
PERIODICAL: Referatlvnyy zhurnal, Elektrotekhnika, No. 3,
1960, P. 37 abstract 2.1172 (Vopr. aerodinamiki
I teploperedachi, v kotellno-topochn. protsessakh.
M.-L., Gosenergoizdat, 1955, 81-99)
TEXT: The process of mixing two immobile infinitely
extending, incompressible gases of an equal density of the
temperatures T 1 and T 2 , respectively, is investigated for
the case that along the surface of division a flat jet stream is
injected which flows from a slot of the width b 0 at the speed
U,; Based on the solution of Hertler, a solution can be found
f the thermal problem if two assumptions are made on the
coefficient of turbulent heat exchange. The temperature .profilesv~
and the expressions for the specific heat flow through the
division boundary and the local and average coefficients of heat
transfer are given. Under turbulent conditions of flow the
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22911
5/112/60/000/003/001/002
Turbulent H-eat and Mass Transfer ... E073/E335
latter amounts to about U 0 and under laminary conditions if
amounts to U 2/3 . The investigated problem of jet movement
of a compressibie gas is reduced to comparing the results of a
theoretical solution obtained by the author 'with other solutions
based on various assumptions concerning the similarity of the
individual fields. Comparison of the results with exp*r-iment
appears to support the hypothesis of the author on the similar-
ity of the fields of density and heat content of an impulse flow
and against the hypothesis of the similarity of temperature pro-
files and of speeds taken separately. Views are expressed on the
redistribution of the total energy in a gas flow in absence of
heat exchange with the external medium* Due to the fact that the
turbulent Prandtl number is less than 1 , fast streams are en-
riched with energy at the expense of slow ones. This phenomenon
is illustrated by results of experiments on the measurement of the
coefficient of recovery and the effect of Rank-Kilsh tubes.
(Abstractor's note: complete translation.)
Card 2/2

REZNYAKOV, Aleksandr Borisovich, prof., doktor telhn.nouk; VULIS. L,A.,
prof., daktor tekhn.nauk, otv.reId.; OSADCHIY,
RCROKIRA, Z.P., tokhn.red.
(Similitude method,, essential features and practical application)
Metod podobiia; sushehnost' i prakticheakoe primenenie. Alma-Ata,
Izd-vo Akad.naulc Enzakhakoi SSR, 1959. 150 P. (MIRA 12:12)
. (Dimensional analysis)

PHASE I BOOK EXPLOITATION SOV/5290
Soveshchanlye po prikladnoy gazovoy dinamike. Alma-Ata., 1956
Trudy Boveshchaniya po prikladnoy gazovoy dinamike, g. Alma-Ata., 23-26 oktyabrya
1956 g. (Trarxactions of the Conference on Applied Gas Dynamics, Held in
Alma-Ata: 23-26 October 3.956) Alma-Ata., Izd-vo AN Kazakhskoy SSR.. 1959.
233 P. Errata slip inserted. 900 copies printed.
Sponsoring Agency: Akademiya nauk Kazakhskoy SSR. Kazakhskiy gosudarstvennyy
universitet ineni S.M. Kirova.
Editorial Board; Resp. Ed.: L.A. Vulis; V.P. Kashkarov; T,P, Leontlyeva and
B.P. Ustimenko. Ed.: V.V. Aleksandriyakiy. 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.) SOV15290
COVERAGE: The bo3k consists of the transcriptions Of 31 papers read at the
conference on gas dynamics which was convened under the initiative of the
Kazakhokiy gosudarstvennyy universitet imeni S,M, Kirovs. (Kazakh State Univer-
sity imeni S.M. Kirov) and -the Institut energetiki Akademii nauk Kazakhskoy
SSR -Uatitute 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
"Transactiond'of 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 joapers read at the Conference are not included
in thib collection for various reasons. The authors of themissing papers
are: L,D, Llvov (Thermal and Aerodynamic Characteristics of Pulverized Coal
Flame Burners) and A,A, Goloyevokiy (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. Yakubav. L.G. Loytoyanskiy is
mentioned as being in charge of a department of the Kazakh State University,
and I.D. MalyWam, Candidate of Physical and Mathematical Sciences, Docent,
as a member of the same university. '.1eferences are found at the end of
most articles.
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Transactions of the Conference (Cont.) SGV15290
TABLE OF COI?rWrS:
From the Edttors
Session of October 23, 1956
Abramovich, G.R. [Doctor of Technical Science&; Professor; TaIAM
imeni Baranova ('central Scientific Research Instituto of Aircraft
Engines imeni P.I. Baranov); Moskovskiy aviatsionnyy institut imeni
Ordzhonikidze,, 14oskva (Moskow Aviation Institute imeni Ordzhonikidze,
Moacow]o Turbulent Jets in a Flow of Liquid 5
Ginzburg, I.P. (Doctor of Physical and Mathematical Sciences;
Professor; Gosudarstvennyy universitet imeni Zhdanovap Leningrad
(State University imni Zhdanov, Leningrad]. On the Outflow of
of Gases From Containers Through Pipes in the Presence of Friction
and Local Resistances 17
Card 319

Transactions of the Conference (Cont.) SOV/5290
Vulis--LA.. [Doctor of Technical Sciences; Profes3or;
Kazakhskiy gosudarstvennyy universitet imeni Kirova;
Institut energetiki Ali Kaz83H, Alma-Ata., (Kazakh State
University imeni Kirov; Institute of Power Engineering
Academy of Sciences Kazakh SM, Alma Ata)]. Basle Results
and Further Problems of Investigating Jet Motion of Liquids
and Gases 29
Ioatayev, S.I. On the Turbulent Wake Behind a Poorly
Streamlined Body 39
Contents of the Discussion in Brief
Session of October 24, 1956 (Morning)
44
Antonova, Investigating Turbulence Characteristics of a
Free Nonisothermic Jet and an Open Flame 45
Kashkarov) V.P. [Candidate of Physical and Mathematical Sciences].
On Parallel and Contrary Motion of Two Uniform Flows of ComIressible Gas 55
Card 4/9

Transactions of the Conference (Cont.) SOV152%
Leontlyeva., T,P, (Candidate of' Technical Sciences]. ':xpansion of
Axially Sy=etrical Jets in Parallel and Contrary Flows 62
Bukhman, S.V. Regularity of Motion and Combustion of Coal Particles 69
11azarchuk, M.M., and NJ. Pollskly. On the Crinia in the Viccous
Flow of Gas in a Plane Parallel Channel 69
Contents of the Discussion In Brief
Seasion of October 24, 1956 (Evening)
75
Terekhina, 11.11. Expansion of an Axially Symmetrical Jet of Gua in a
Medium of Different Dencity 77
Chebyshev, P.V, (Vaesoyuzn-,y elektrotekhnicheE;kiy inatitut (All-Union
Electrotechnical Institute)), Electrothermoanemojmters and Their
Use in Investigating Nonisothermic Gas Flows 85
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Transactions of the Conference (Cont.) SOV15290
Trofimnkop A.T. Inveatigating a 3emireatricted Turbulent Jet 100
Akatnov, N.I. Survey of the Works of the Department of Hydroaero-
dynamics of the Leningrad Polytechnical Tnstitute imeni Kalinin
on the Jet Theory 107
Shepalev, S.F., and S, Tsoy, Plane Jet in a Cross Section of an
Air Conduit 108
Bespalova, V.G, Use of Hydrointegrators For Solving Jet PrLblems 115
Contents of the Discussion in Brief 122
Session of October 25, 1956 (Morning)
Katsnelloon,, B,D, (Candidate of Technical Sciences; Docent; Tsentralinyy
kotloturbinnyy institut imeni Polzunova,, Leningrad (Central Turbine and
Boiler Institute imeni Polzunovp Leningrad)].
Some Problems of the Aerodynamics of Furnace Cyclone Chambers and of the
Combustion of Coal Powder Pulverized Coal 123
cara 619

Viransactiorn o' the Conference (cont.) BOV15290
Ustimenko, B,P, Candidate of Technical Sciences,, Aerodynamics of
an Involute Jet and of a Cyclone Chamber
Volkov, Ye. V. Sow Aerodynamic Problems of u Two-Mano Flow in
a Cyclone Furnace
Tonkonogly.. A.V., and I.P. Bas1na, On the Problem of the Working
Process in a Cyclone Chamber
Yakubov, G,V. Generalizing Aerodynamic Lave of Cyclone Chambers
Contents of the Discussion in Brief
Session of October 25, 1956 (Evening)
Reznyakov, A.B. (Doctor of Technical Sciences; Institut energetiki
(Institute of Power Engineering)). Uniflow Flame of Pulverized Coal
Telegin, A.S. Reg4arities of Gas Flame Burning
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134
142
152
158
158
:L60
160

Transactions of the Conference (Cont.) S0715290
Yershin, Sh. A. Acrodynamica of a Turbulent Gas Flame 168
Kokarev, M, [Candidate of Technical Sciences; Urallskiy
politekhnichookly institut imeni Kirova, Sverdlovsk (Ural
Polytechnical Institute iment Kirov, Sverdlovsk)], Industrial
Testing of New Gan Heads of Open Hearth Furnaces 178
Bogdanov, Ye, P, On the Thermal Regime of the Gasification Process 186
Contents of the Discussion in Brief 186
rinal Session, October 26, 1956
Zhulayev, P. Zh. [Candidate of Technical Sciences; Docent],
Survey of Work on Hydrodynamics Done by the Institut Energetiki
AJI KazSSR (institute of Power Engineering of the Academy of
Sciences Kazakhakaya SSR) 187
Romanenko, S.V. (Deceased). Basic Problems of Flow Tbermodynardcs
in Real Boundar-.1 Conditions 197
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