SCIENTIFIC ABSTRACT PERELMAN, R.G. - PERELMAN, T.L.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001240010013-9
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: June 15, 2000
• Sequence Number: 13
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

ri~jr.
S/281/63/000/0.01/004/004
41;r. :~X:
1:-th,eory of the'
from the pump to-the t6ta.1 drive -power., Separate
th equation as them
z_axv~ezz ions i are derived for' such cc, ponents of 0
hy4-r~aulic -efficiency,- the'fricti the,
onal head and others, BO that
res-41tilag -46 Lat ion rformance is complicated though
qu or pump
pe
'."Usaple Anal siB of the expressions derived shows tl~at there is
'y
-6pticuum vulue_of fluid.:fr4ction'against the disk which gives
-plaij mum iciency.. In practice, the'. best results are
-bbtained dizk~sectlons fIl1o.4_o.5 of the Inlet. section.,
5'Th~i 6nco~
'influi mp design 'and~geometry--on,performance is then.
PU
corls der"e-d.i'xiid-performanco~curves-are cons
y tructed for-pumps of.
A gi-slen designsi A special rig was built in which the spacing
b-dVve4n disks could be in the- ranye 5 - 9 mm, the coefficient of
_~2 0 77, s' - 7000 rpmt,.the discharge.
ion 0.0 the pped'3,000
dil
xyrjeter~ 10C 500 mm, and. the height of roughnesses'on the disk
s
T'face (vrhJ.ch influences the Reynolds number in th gap)
u,.C
.0.005 0. mm. There :is good &jVeement between experimental
b racteristics 'obtained on :this rig ;knd calculated values,
provided th4tithe specific'speed IB' greater than 70 80. If it
-1e -values of efficiency and. head are lower
i81 ss, tho experimental,
culated. -There are:12 figures,
'~rd SUBMITTEP i Ju'ly 6, ~l 61
C

PHASE I BOOK EXPLOITATION SOV/6204
Perellman. Roman Grigorlyevich
Dvigateli galakticheskikh korabley (Engines for Intergalactic Ships) Moscow,
Izd-vo AN SSSR, 1962. 197 p. (Series: Akademiya nauk SSSR. Nauchno-
populyarnaya seriya) Errata slip inserted. 25, 000 copies printed.
Sponsoring Agency; Akademiya nauk SSSR.
Resp. Ed.: K. P. Stanyukovich; Ed. of Publishing House: N. B. Prokoflyeva;
Tech. Ed.: S. P. Golub'.
PURPOSE: This book is a popular treatment intended to acquaint nonsppcialist
readers with various engine design concepts for use in intergalactic ships.
COVERAGE: The book gives Information on interstellar "routes", discusses
the principal limitations of rockets with engines using chemical and nuclear
fuels, and--presents the basic concepts necessary to an understanding of
Card 1/0,

PEM I DDDX Eawx=ox SUV/5703
Perelfman,, Ronan Grigorlyevich, Candidate of Technical Sciences
Shtum kosmosa prodolzhayetoya (The keesult on SWe Continues) NDscOwt
I2d-vo "Enanlyep" 1961. 44 p. (Berleal Yeasoyunoye obobehestvo pD
rasprostranemlyn politicbeekikb i.mmcbnykh rumnly. Serl7s, IX,, 1961:
Fizilia I kbinlya., noo 13) 26,,000 copies printed.
Edo: 1, B. Faynboym; Tech. Edo: A, So Nazarova,
MPOSE: This booklet Is Intended for the general reader,
COVERME: The booklet reviews the developwnt of Soviet exploration of outer
space and describes aspects of recent Soviet achievements,. Propulsive
efficiencies, velocity requirementep rockets., guided rocket vehicleBy
satellites, the satellite capsule., launching, control, pover systems, and
atmospberic entry are discussed& References to future possibilities and
trend.s are made throughout the booklet. A few Illustrations are included.
No personalities an mentioned, There are 26 references., all Soviet,
Carr: 11,2

FEMINANO Roman ;Grii~gorv b; STANYUKOVICH, N.V.. prof., otv. red*;
. yevlic -
-------7AUKUFM , I.B., red. izd-va; GOLUBI, S.F.,, tekbn. red.
. x
(Engines of galactic ships]Dvigateli galakticheskikh korablei.
Moskva.. Izd-vo Akad. nauk SSSR, 1962. 197 p. (MMA 15:9)
(Spaceships-Propulsion systens)

FERELIMM p Waman GrimprOyevich.kand. tekhn. n*k; FAMOYMt I.B.9 red.;
-qr,46.-i~ed. ---
(Assault on outer space continues) Shtum kosmDoa prodolsbastalao
Hol*UP lzd-vo "UanievO 1961. " po (Ysevolume obsbabestvo po
raisprostr"nliu politicheskikh i uauchnykh mAnils Sao% Fizika
I Wdmilag-,no.13) (NDU 1416)
(Space f3.igbt)

M4SE I BOOK EXPLOTTATIOW SOV/5686
Perellman., Roman Grigorlyevich
Zvezdnyye korabli (Stellar Ships) Moscow, Izd-vo "Sovetskaya Rossiya," 1961.
61 p. 20,000 copiea printed.
Scientific Ed.: G. I. Babatp Doctor of Technical Sciences, Professor;
Ea.: W. Ts. Stepanyan; Ed.: E. Rozen.
FURPOSE: This is a popular booklet for general readers.
COVERAGE: TbLe booklet deals with problems in the development of astronautics.
Prognosis for the future and the scientific basis for building spaceships
are given on the assuzption that -the development of astronautics will foll'y';
the lines being laid down by science at the present time. Soviet and non-
Soviet open sources were used. No personalities are mentioned. There are
no references.
Card-1/3-

PMMINAN,- %, STANYMVICH, K.
Ut's be optlvistlcl'Zrmn.Rllft 15 no.7t38-40 Ji 060.
(KrM 13:7)
(Spaca flight)

S/024/60/000/04/003/013
E/194/E484 82207
A137HOR: Perell-man, R.G. (Moscow)
THLE; Ihe Selection of Optimum Parameters for an Injector-
PuTk Runner System
PEFIODICALt IzvesAiya Akademii nauk SSSR, Otdeleniye tekhnicheskikh
rauk, Energetika i avtomatika, 1960, No-4, PP-59-73
TEXTt The method developed by TsAGI (Central Aerodynamic and
Hydrodynamic Institute) for the design of fans can be adapted to
determine the optimum inlet diameter of a pump runner to achieve
mir.imum inlet pressure lose. This makes approximate allowance
for rotary motion that is set up in fluid that has not yet reached
the,-runner. I'he anti-cavitationlpropertieB of the equipment may
be further improved by means of an ejidtor, such as that
illustrated-schematically in Fig.lj in which part of the head
ave.i-lable before-the-nozzles is used to aet up axial flow and for
e-jeet-ion-, and another part to set up rotary motion of the fluid
before entering the runner. The fluid for the ejector is taken
from the high-pressure part of the system. The object of the
Present article is to determine the optimum distribution of the V~
heaA available before the nozzle of the ejector to set up axial
Card 1/6 V>

S/024/6o/ooo/o4/003/013
EIL94/3484 82207
The Selection of Optimum Parameters for an Injector-Pump Runner
System
arid peripheral velocity in the ejector-pump system. The angle
of the nozzle in the horizontal plane P2 in Fig.1 is first
considered. Tests have shown that for small values of P2 the
flow rotates mainly near the chamber walls, but when P2 - 45 0
the rotary motion is reasonably well distributed. On the other
hand, increase of 02 above 45* reduces the rotary rate of flow.
Ruperimentally determined values of the two velocity components
for different values of P2 are plotted in Fig.2,and Fig.3 shows
velocity diagrams across the radius for three different values of
P.2- It is seen that a value of 02 Close to 45* is the most
favourable. The generally accepted equation for determination of
the head required at inlet to the set (in the absence of an ejector)
drawn up for flow conditions on the outer diameter of the blades,
where cavitation is most likely, is given in Eq.(2). The ejector-
pump systen. is then analyzed further to derive the necessary changes
in Bq.(2) and the optimu inlet diameter in the presence of a shaft
in given ty- Jtq.(4), or in the absence of a shaft by Eq.(41). The
use of an ejector which sets up an additional head and rotates the
Card 2/6

S/024/60/000/04/003/013
B194/E484 82207
The Selection of Optimum Parameters for an Injector-Pump Runner
Sy St em
flow causes changes in the expression for determining the total
inlet head, see Eq.(21). Further consideration in then given to
detailed consideration of terms entering into Eq.(2). The
reduction in required pressure that results from reduction in the
relative velocity at the inlet diameter is assessed. The change
in angle of attack resulting, from the rotation of the flow before
the wheel Is discussed in relation with the vector diagram of
Fig*4. Upression (12) is derived for the increase in the
available vtatic head caused by the ejectors. The equation for
the optimun head distribution is then derived in the form of
1q.(15) which may be used to derive various of the necessary
velocities. Analytical solution of Eq.(15) involves the use of
a suall difference between two large terms and great care is
required to obtain sufficient accuracy and accordingly a semi-
graphical method is recommended. The semi-graphical method gives
j;raphs in dimensionless coordinates for the common practical case
Cof an overhung wheel. The construction and use of the graph is
J-11ustrated by an example of selection of the angle of slope of
Card 3/ 6

S/024/60/OORI;04/003/013
E194/8484 07
Tihe Selection of Optimum Parameters for an Injector-Pump Runner
System
the ejector nozzles. The nature of the changes of the various
wignitudes (see Eq.(13) )with constant drop in the nozzle and
various angles of slope of nozzle are plotted in Fig.5 and curves
of' the relative gain in inlet pressure are plotted in Fig.6.
Finally. Fig.7 shows a combined resultant graph of the relative
gaim in inlet pressure, which may be used directly to determine
thet beat ejector nozzle angle. The use of this graph is explained
and numerical examples are worked. see Fig.8, curve 2. It is
shown from Fig.7 that in one particular case the improvement in
anti-cavitation properties of the pump which can be achieved by
using a combined ejector is about 1.2 times greater than that
when all the pressure drop on the nozzle of the ejector is used
to set up swirl. At present, axial ejector-pumps are commonly
used And accordingly an example is given. The combined
resultant gain curves for this case are given in Fig.9.
Uperimental work was done using an incompressible liquid to check
the above recommendations on the selection of optimum nozzle
angles for the ejector in the ejector pump system. The necessary
ca:rd 4/6

5/024/6o/ooo/o4/003/013
z194/1g484 82207
The Selection of Optimum Parameters for an Injector-Pump Runner
System
pasp design date are given. The procedure used to determine the
cavitation characteristics in explained. A cross-sectional
diagram of the pump and ejector are shown in Fig.11. Results are
pl*tted In Fig.10 and It will be seen that, for reasons which are
e:i~plalnedq the increase in static pressure developed by the
9jector van about 5% lower than the calculated figure. There was
a corresponding diminution-in the possible gain. Finally, the
cojobined ejector illustrated in Fig.llb was tested. In this case,,
the pos3ible reduction in the dynamic component of the pressure
roquired at islet was 5 to 6% below the calculated value, for
reisksons which are explained. In selecting the optimum pump inlet
diameter, and so in constructing the graphs of Fig.7 and 9. no
allLowance was made for possible further increase in optimum
diameter caused by swirl of the liquid before inlet to the
runner, This -simplifies the problem but to be sure that the VK
anstumptions do not greatly impair the advantages of using an
oJoictor, an assessment in made of the change in optimum diameter
thait results from allowing for swirl of the liquid. The results
Card 5/6

t jc ~~,Cj_
10(2)(4); 1.4(6)(10) PHASE I BOOK EXPLOITATION SOV/3427
Polikovskiy, Vladimir Isaakovich and Roman Grigorlyevich Perellman
AForonkoobraz.ovaniye v zhidkosti s otkrytoy poverkhnostlyu (For-
matid;n of Funnel-Shaped Depressions In Liquid with a Free Surface)
Moscow, Gosenergoizdat, 1959. 190 P. 1,750 copies prInted.
Ed.: P.G. Kiselev; Tech. Ed.: G.Ye. Larionov.
PURPOSE: This book is intended'for specialists and students of
hydrotechnics, as well as for engineers designing various
kinds of industrial and transportation hydraulic system.
COVERAGE: This book presents the results of titeoretical and
experimental studies devoted to the problem of vortex formation
in the flow of a liquid with a free surface. The book is divided
into two main parts. The first part discusses the physical
nature of' vc)rtices and the method of evaluating phenomena which
arise when a liquid has a vortex. Among the topics considered
are: theory of vortex formation, exptrimenLal study of physical
Card 1/6

Form*tion of Pannel-Shaped (Cont.)
SOV/342T
existence of vortex formation, and calculation and conBtruc"on
of vortex Profiles. Part two discusses vortex formation in
the upper water of hydrotechnical Installations.. Among the
topics considered are: vortex formation in front of looks of
hydrotechnical installations, determination of look stresses in
draining off solid floating objects by means of vortices, evalua-
tion of pez7aeability capacity of hydroturbine spiral chamber's,
prevention of vortex formation, and the use of vortices In
cleaning foreign objects from the surface of reservoir waters.
There are 130 references: 113 Soviet, 6 German, 5 Englisn,
3 French, 1 Hungarian, 1 Italian, and 1 Rumanian.
TA.BLE OF CONTENTS:
Preface
PART ONE. THEORY OF PHYSICAL EXISTENCE AND METHODOLOGY OF
EVALUATING PHENOMENA OF A LIWID DURING VORM FORMATION
Ch. I. Theory of
1. CauseB'and
formation
Card 2/6
5
Vortex Formatton
physical nature of the phenomenon of vortex
7

Formation of' FLLnnel-Shaped (Cont.) SOV/3427
2. Escape of a liquid with non-rotating vortex through a
bottom orifice and the critical state of flow 13
3. Theory of steady vortex formation 18
Ch. I I. Experimental Study of the Physical Nature of Vortex
Formation 39
4. Basic experimental equipment 39
5. Evaluation of the effect of viscosity, discharge of liquid,
disturbing moments, and pressure on vortex formation 41
6. Model 14 ns of vortex formation
.L 46
7. Determination of discharge coefficients during escape
throai;h a circular bottom orifice with a vortex over it 49
8. Approximate value of the possibility of a vortex break in
a bottom orifice 53
9. Experiments on the prevention of vortex formation in a
cylindrizal tank during escape through a bottom orifice 55
:,0. Vortex formation in a side discharge 61
..l. DrainIng of solid floating bodies by vortices 70
Ch. I II. Macite.r Calculations and Construction 76
Card 3/6

Formation of Funnel-Shaped (Cont.) SOV/3427
12. Deteimination of calculation coefficients 76
13. Methodology of constructing the calculation prufile of a
vortex 83
14. Numerical example of constructing a vortex profile 86
PART TWO. VORTEX FORMATION IN UPPER
WATER OF HYDROTECHNICAL INSTALLATIONS
Ch. IV. Vortex Formation in Front of Looks of Hydrotechnical
Installations.
15. General considerations on the causes of formation of
vortices and their intensity depending on the elevation
of the lock 91
.6. Appro;Umate constructlon of the form of the flow surface
before tlie lock 95
-7. Quant'.-tative evaluation of the intensity of the vortex
befom! a lock. Examples of calulcation of vortices 98
18. Experimental determination of the distance of a vortex
from look on a model and in actual practice 103
Card 4/ 6

Formation (-)f Ftairle I - (0'. rIL . 11 SOV/3427
19. Obliervati,~rs in actual practice of spontaneous vortex for-
ination arid tne effect 3f draining solid floating bodies
by vortices 103
01h. V. D**.-tE:nni.n&tl-r1 t,f )n Locks in the Draining of
Solid Floating Bodilea (logs) by Vortices 106
20. Preliminary conA-Ae rat. 1 on6 1o6
21. Reialts of A)j,::.-Nationj and characteristic caues of calou-
lation 109
22. Deteiinlriatlun of Ur,,,: .1iitL,aot, I )x-c,- of a solid body on the
lock (ca.,-Je A-1), 113
23. W, termlratl,)n -)f -)n tni:: lower edge of a lock
(case B--2) l16
24. Eximildeb ,f val,-,alatin,., a-1,11tional i3tresses on locks 119
Ch. VI. Evaluatlin of Per-YrLeability Capacity of Spiral Chambers
of HydrotiLrbines 122
25. General considerations 122
26. Maximal d1scharge during escape in the form of a developed
vortex 126
Card 5/6

Cl Cl I
Ch L I -,to:
er Intakes In
loakz,
c h
an 1
B3
AVA 1, LA L)LF, L:
155
17~
AC,'j b
C a Y, 1 0 t7, 4-8-0"o

10V
0 /:"5-59-,", - P 7/49
AUTHOR: Perellman, R.G., Candilate of Technical 'cie7.c-s
T ITLE: The Attack on the Thermal Barrier
F ERIODI CAL t Nauka i zhizn), 1959, Nr 6, Pp 59-64 and P 3 of centerfold
(1)SSR)
AB")TRACT: This is a popular introduction into the problems connected
with the attempt to overcome the so called thermal barrier,
i.e. the sharp increase in heatinf~ up of the aircraft during
flight, and the increaslnC difficulties connect-d -,,,ith
inC, hi(:h speed aircraft. The author deals first %%-ith the
aound barrier and how it was overcome, and then describ-s
an imagined flight of 4,50C km/h at a height of 11 V-Tn. He
sets forth the difficulties arising because of the ii,tensive
heating up of the aircraft, statine that a further rise in
spiied will requirc the increased use of heat-rr.,siste~nt
stacls. It will aloo be necessary to develop new i-tho's
and instruments for the processin(7 of materials in er.er to
enoure the hiGh productivity of the aircraft industr.y -.,.-ith
Card 1/3 such steels. It is evident that the materials select,~j for

SOV/25-59-6-27/49
The Attack on the rhermal Barrier
the building of aircraft ohox.ild bf- aa littlo an ponziiblr silb-
jected to dimensional changes due to toriipnratur~-. Th'3 Ruthor
refers to the US experirental aircraft "X-15" des-.UneJ for
training flights at super-sonic speeds. However, the select-
iort of suitable conotruntion naterial3 does not solv- the
entire problem ainoo the) aircraft aloo holdti tanho with flAol,
numerous devices and a human beinp. The difficultieg experi,-n-
ced in this connection tire also set forth. The author deals
witb the possibilities of "keepin,- off" the heat by mnkin~_-
a "sweating" skin of porous, non-rusting steel. The autiior
also mentions other known methods lea~ling to a protection of
the skin against hi[-h temperatures, such as a skin of materials
which only poorly conduct heat, are fireproof, or let the
hot air rotate the turbine wheel of a special refriU.?rator.
Examining the prospects for the future, the author points to
the possibility of maneuverin,-, i.e. to fly at a inaXIMUM 0
speed until the aircraft ;kin is heated up to about 400 C,
then reduce the speed radically to let the aircraft cool off
Card 2/3 and thereafter increase the speed arain. He hints at in~,reas-

SOV/25-59-6-27/49
The Attack on the Thermal Barrier
ing the aircraft's altitude as another way of meFtinC the
difficulty. It will permit the airoplane to fly at a speed
of about 10,000 kn/h at haiChts of 100 to 150 km for ~;evpra`
hou:7s without overheatinj,. Concluding, lie ~itatns that thruu~-~l
the endeavor3 of en(;incers, degigner,,, physicist3 and chemists
aircraft will from year to year be able to fly fa,-ter,
farther and higher. There are 11 sets of drawings and 1
graph.
Card 313

.PZHIT IwIf_.A-G-,k-and.tekhn.nauk
Nuclear transport. Politakh.obuch. no.6:66-79 Je 157.
(HIRA 12:4)
(Nuclear engineering)

KOU13VSKAYA, A.Ye. kIRILIKAN. -R.G. (Hoskva).
Hoat exchange in the field of action of centrifugal forces.
lim. AN SSSR. Otd. tekh. nauk. no.11:92-94 X '58.
(MIRA 12:3.)
(Eleat-Transmission) (Centrifugal force)

SOV/124-57-9-10349
Translation from: Referativnyy zhurnal, Mekhanika, 1957, Nr 9. p 66 (USSR1
AUTHORS: Poliloovskiy. V. I. , Perel' man, R. G.
TrrLE: The Evaluation of Loads on Water Gates Due to Floating Solid Bodies
Sucked Into Whirlpools (Otsenka nagruzok na zatvory pri podsasyvanii
voronkami tverdykh plavayushchikh tel)
PERIODICAL: Tr. MAI, 1955, Nr 50, pp 216-230
ABSTRACT: The paper submits the results of investigations on the evaluation
of possible additional loads on water gates due to solid floating bodies
(logs) sucked under by whirlpools. The investigations were conducted
in the hydraulic flume on a model of the spillway dam of the Kuybyshev
Hydraulic Power Plant built to a scale of 1:50. Whirlpools were
created in the corners between the gate and the pier by means of a
tangential delivery of water through an eddy stimulator. The basic
laboratory tests were made with two values of the opening of the
gate a/ H=0.25 0.30 and 0. 5. The Reynolds number was expressed
as R = rCu/-y where Cu was the peripheral velocity at a radius r.
Round wooden logs were used as models of the floating bodies. A high-
Card 1/3 speed motion-picture film was made at 80 frames per second.-Xhe

SOV/124-57-9-10349
The Evaluation of Loads on Water Gates Due to Floating Solid Bodies (cont. )
te!.ts were analyzed by the consecutive projection onto a screen of the single
motion-picturia. frames and the positioning of the moving body upon a coordinate
grid every 1/80 of a second. Floats entering in the hollow of a vortex and observed
by means of a stroboscope , as well as on the coordinate grid, made possible an
evaluation of the intensity of the whirlpool. The authors also conducted full-scale
observations on the suction of floating objects into the whirlpool under the water
gates of the Ivankovskaya dam. On the basis of the investigations made, as well
as of investigations made by other authors, two typical cases of the motion of a
log before a gate were established: A)When the whirlpool does not have the inten-
sity required for sucking a body under the gate, and B) when the whirlpool sucks
the body under and carries it out under the gate. In the first case (direct impact
of the log against the gate), assuming that the impact is absolutely inelastic, the
impulse of the force is determined as equal to N = 0.8mv with a = 450 and N = mv
w,th a = 00 and 90o, where a is the angle between the direction of the log and the-
normal to the gate. Since the greatest specific impact loads occur with a = 06
(head-on longitudinal impact by the log), this impact condition is the most dangerous.
1r this load condition the mean value of the force during the time of the impact is
P _n mv
Card 2/3 T 2J 3,yT/ E9

SOV/124-57-9- 10349
The Evaluation of Loads on Water Gates Due to Floating Solid Bodies (cont. )
In the second case, if the log, because of its large size and an insufficient intcns~ty
of -.he whirlpool, is not carried away by the latter at once, but rotates vertically,
goes down along the gate, and accomplishes a turn around the bottom edge of the
gate, then the force acting upon that edge is determined by the expression
N = 0..%c P s V2 = 0.5 c p (I - h) D v2
At the end of the article two examples of design calculations are given. The authors
did not analyze the significance of the described load on the gate in comparison with
the design load (hydrostatic pressure). Bibliography: 9 references.
A. P. Berezinskiy
Ca:.-d 3/3

SOV/24-58-10-30/34
AUTHORSiLe~l'man, R. G.,, Polikovskiy, V. I. Oloscow)
TITLE: I~ydraulic Imp;-d~ce of Rectilinear Channels in the Field of
Centrifugal Forces (Gidravlicheskoye soprotivleniye pr,-y-amol-
ineyr~ykh kanalov v pole tsentrobezhnykh sil)
PERIODICAL: Izvestiya Akademii nauk SSSR, Otdeleniye tekhnicheskikh
nauk-, 1958, Nr 10, PP 150-153 (USSR).
AB3TRACT: A determination was carried out of the hydraulic impedance
of smooth brass tubes whose internal diameter was 10, 20 and
28 mm. The tubes were placed radially in a plane which was
at right; angles to the axis of rotation. Experiments Lvere
carried out in air up to Reynolds numbers R - 7 x 10-a~ .
The experimental results are shown in Fig.1, in which the
frictional loss coefficient X is plotted as a function of R
and the angular speed n . An expression is derived which
gives the hydraulic impedance as a function of the parameters
of the tube and the rate of revolution (Eq.6). There are 4
figures and 7 references of which 3 are German and 4 Soviet.
SUMITTED: July 27, 1957.
Ca2-d 1/1

PHASE I BOOK EXPIDITATION 527
Perellmanp Roman Grigorlyevich, Candidate of Technical Sciences
YeierMye dvigateli (Nuclear Engines) Moscow., Izd-vo "ZnanVe*j, 1958. 54 p.
(series: Vsesoyuzvoye obshchestvo po, rasprostranenlyu politicheskikh I nauchnykh
maniy. Seriye. IV., 1958., no. 4 and 5) 60.,ODO copies printed.
Scientific Ed.: flikolayev, N. A.; Ed. of Publishing House: Lanina,, L. I.;
Tech. Ed.: Stzvletskiy,, I. A.
PURPOSE: The*booklet is intended for the general public interes-ted in future
developments in the field of atomic energy.
COMAGE: The auflior describes in popular language tie porspecto for utIlizUs
atomic energy,, particularly in the field of transportation. No precise de.
scrit.plon of transportation facilities in the atomic era can as yet be given.
7he Soviet Unicza has accumlated considerable experience in the continuous opera.
tion of industrial nuclear electrie power plants. The Sixth Five Year Plan oalls
for new nuclear engines and new larger electric pover plants, and nuclear Ice-
breakerep one of vhIch Is now almost completed. The author describes the ad-
vantages of inatallations of power plants operating on nuclear fuel. He eltes as
Card 1/4

Nuclear Ragines
527
an example the renent, Soviet achievement in launching December 5, 1957 on the River
Neva the nuclear Icebreaker "Ienin",, vb1ch is 134 m. long, 27.6 m. wide, 16 m. high,
ani has a 16pODO ton displacement and a speed of more than .30 km. per hour. The
ioebreaker Is equipped vith launches on its deck and a helicopter on a special plat-
fom Its nualear engine produces more than 40,ODO horsepover. The potential do.
sl~gns of ran Jets operating on nuclear fuel are under study.. Le.~ the VRD (Jeta)
anit the TED (74rbojets). The future vill bring nuclear space ships and the use of
caitrolled themmiuclear reactions. The discovery of a method for controlled trans-
fo-.-mtion of matter into energy in quantum engines will open nev cosmic perspectives
In rocket techaique. Photon and ion rockets vill 'be used in the future. V.V. Zvonkov,
Corresponding Ifttler of the USM Aeadewl of Sciences, is mentioned as the person Vho
sujMrvised the vork on nuclear-povered tankers of 15,ODO hp. There are 23 references,,
of thich 18 ar3- Scrv:Let,, 4 English.
Card 2/4

Nuclear EAginee 5 27
TAIIIS OF
COMEM:
The Ragine of the Future
Across the 3ine: Seas 10
E4;hty Thousand X11ometers Under Water 1T
7he Incowative of Deserts, Distant Roads, and Mmwtain Passes 21.
On the Higbvay of the Atomic Era 29
Around the World 31
The Atom Acquires Wings 38
Itaclear Rot*et a 42
Curd 3/4

Na,*.Iear Engines
Conclusion
Bibliagraphr
AMMABLE: Librmy of Congress
C&rd 4/4
527
IS/eag
9/25/58
53
54

AULORS: Kovalevskaya, A. Ye. andP SOV/24-58-11-21/42
!~r~~~Ian, R. G . (Moscow)
TIPLE: On the Heat Exchange in a Field Affected by Centrifu6al
Forces (0 teploobmene v pole deystviya tsentrobezhnykh sil)
P&RIODICAL: Izvestiya Akademii Nauk SSSF, Otdeleniye Tekhnicheskikh
Nauk, 1958, Nr 11, pp 92-94 (USSR)
AB13TRACT: M, A. Mikheyev (Refs 1 and 2) studied the heat release
from heated rotating rods to the atmosphere (external
problem). In earlier work (Ref 3) the authors of this
paper studied the heat flow inside a canal (internal
problem). The investigations described in this paper are
based mainly onthe results of this earlier work and relate
to determining the hydraulic resistance of straight caniils
inside a field affected by centrifugal forces. Various
authors have published formulae enabling inter-relation
in the first approximation of the heat transfer coefficient
a and the Nusselt number NNu* The possibility of usin6
the relations published by Ludwieg (Ref 4) and
Kutateladze (Ref 5) (Eqs.l and 2 of this paper) are
determined by the extent to which the heat propagates in
the flow along the investigated section. In the
Cai-dl/3 exPeriments carried out by the authors of this Daper the

SOV/24-58-11-21/42
OIL the Beat Exchange in a Field Affected by Centrifugal Forces
lenE;th of the ring section in which the heat transfer was
effected consisted altogether of two tube sizes and it
can be anticipated, therefore, that the experimental
results in the investigated region andthe applied length of
the heated section will be
intermediate relative to those calculated according to the
f ormulae of Ludwieg and of Kutateladze. A sketch of the
used experimental set-up is shown in Fig.3. It was found
that the experimental results are in satisfactory agreement
with the theoretical relations plotted according to the
foriaulae of Ludwieg and Kutateladze. It can be seen from
the graph, Fig.2 that an absolute decrease in the flow
rate, i.e. of the NRe criterion, will bring about an
increase in the difference between the experimentally and
the theoretically determined valuoa and tho exporimentally
obtained coefficients will be larger than the calculatec
values. This is possible due to the relative increase in
the intensity of the secondary flows in the case of
Card2/3

SOV/24-58-11-21/42
On the Heat Exchange in a Field Affected by Centrifugal Forces
decreasing values of the ratio "Re to N 'Re'
There are 3 figures and 5 references, 4 of which are
1 1 German.
Boviet,
IJUBMITTED: December 31, 1957
Card3/3

kand.takhn.nauk
-,1'-"s.-- - -, 1 - "'
Motors for Galactic ships. Nauka I zhign' 25 no*7'60-64 Jl '58.
(Space flight) (MIRA 11:9)

124-57-1-531
Translation from: Referativnyy zhurnal, Mekhanika, 1957, Nr 1, p 66 (USSR)
AUTHOR: Perellinan, R.G.
Ti TL E: Investigation of the Phenomenon of Funnel Formation (Issledovaniye
yavleniya voronkoobrazovatiiya)
PE-RIODICAL: Tr. MAI, 1954, Nr 38, pp 100-149
ABSTRACT: The study is devoted to the problem of the formation of a
funnel during the outf.low of a liquid from a cylindrical container
through a circular opening in its horizontal bottom. In the
experimental apparatus the funnel was artificially created by
means of a whirling motion produced by concentrated jets which
%&ere tangentially injected into the container. In his examination
of the motion during the stationary outflow of a viscous liquid,
the author assumes that part of the head is expended in the
maintenance of the whirling motion of the viscous liquid, and
that only the remainder of the head is expended "in producing
the discharge, " The autho. assumes the following law for
the distribution 61 the peripheral velocities cu in the flow of
Card 1/~ the whirling viscous liqiiid: rx c- const ,

124-57-1-531
Investigation of i:he Phenomenon of (c ont
where r is a radius and x is a head-loss coefficient comprising the energy
iosses due to internal fricti6n and the friction with the walls and bottom
of the container. This coefficient is determined experimentally. The author
also proposes a formula for the approximate calculation of the pressure
6stribution in the presence of a funnel Regarding model tests of the form-
ation of a funnel, the author concludes that the determing influence therein
is exerted by the viscosity; hence model tests must conserve the Reynolds
number, which is expressed as follows: R = r cu/%r - The determination
cf the discharge coefficient in the presence of a funnel is also examined. In
conclusion a numerical example of the tracing of a funnel profile is set
f:)rth.
Edbliography~ 7 :references
O.F. Vasil'yev, N.A. Pritvits
Liquids--Flow--Analysis
Card 2/2

1UTHOR- F-Brellman, R.G., Candidate of Technical -Sciencee
IITLE: A Window to the Future (11kro v budw;hcheye). The Engines
of Spaceships (Dvigateli 9&IAktiche#flcJIrh korabley).
PERICDICAL: Nauka i zhizn', 1958, Nr 7, pp 60 - 64 and 3 of inner foA,
(USSR)
are 4 drawings.
OSTRACT: Fiction. There
I. Spaceships--Propulsion
Card 1/1

SIITBYN, 16.11. jeningrad); PIMIMUI, R.L., professor, xaveduyushchly; SEMOV.
A.D. dotsent, direktor.
Studies on the active tomis nf the lungs with simltuneous bilEtteral water
-nometry. Arkh.pat. 15 no.1:45-50 J&-F 15), (HLRA 6:5)
1. Otdol ek%perimentallnoy patologit Laningradskogo tuberkaleznogo insti-
tuta im.A.TIL. Shternberga (for Perel'-,mn). 2. Leningradskly tubarkuleanyy
institut im, c~.Ta. Shternberga (for Somenov), (Umgs )

SHJTSKAYAv Ye.l.,, kand. mod. nauk; Prinimli uchastiye: RABINOVICH,
S.Ye., prof.; SLEPTSOVA, A.I., vrach; LIM, K.I., vmch;
SOKOI07A, R.I., vrach; FERELI'W, R.M., vrach; AWTHM, I.M.,
vrach; SEFP.UDV, N.S.9, kand, veterin. nauk; SVIRIDOV,, A.A.
Epidemiological inportance of tuberculosis in cattle.
Veterinariia 40 no.10tl9-20 0163. (MIRA 17:5)
1. Novosi)Arskiy nauchno-iseledovatellskiy inatitut tuberkuleza
(all except Sbepilov, Svirldov).

CHERENITYKH, L.P., ~-arld.med.nauk; FEUELIMANJI-A9~N'..- - ~
ClIn'.comorphological comparison3 in ch.-cnic pi-imax-y tllco~'-Irs'a 2f
the -j.ung;3 in children. Frobl. vab. rj~-.2a74-~q I ~,,.
' I
~141 RA 17 , 12 )
.1. Novosibirskly nauchno-IsBledovaLellskiy institut tuberkuleza
(dir. M.V.Svirpzhav).

FEOFILOV, G.L.; PERELIMANI R.M.; KHRAMOVA., L.P.
Brorichological examination of children with chronic pulmo ar
'losis. Probl. tub. 1.2 no.1:16-21 '64. n y
tulwrou. (MIRA 17:8)
1. Institut eksperLmentallnoy biologii i meditsiny (dir. 7u.1.
Borodin) Ministerstva zd-avookhraneniya RSFSR i Novosibirskiy
nauchno-issledovatellskiy institut. tuberkulaza (dir. M.V. S
Svirezhev).

Azerbaijan State MeAcal Library of the Knistry of Public Healtb
of the AserjaijanS.S.R. Axerb. med. shur. no.11871-73 N 160.
(MIU,13:12)
1. Ispolppyushohiy obyammoati direktorA'Amerbaydshanskoy gosudar-
stvannw.r nauchnoy meditsinskoy biUlioteki Minieteretva sdravookhranoniya
A%evb%ydzhwwkoy SSR.
(AZERUIAN-MEDIUL LIBRULTES)

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au Ow 114110. 10mvit it suf1kwnt tim, 1,,
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00 17. No. 6. 3-90 of NOv and N10a dt-
00
00 twods on tim tIWA=P% M WAS. and on prcvwtc.
:;o
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00 bdom oboorpson=l 6 atm. the rate of the reactims is
00 so raW slat It &rs not binds- abonwion of N%. In
N&jC% Kim.. N&% b ittembed tamer than NCst. Tbtw
solm. mum ectistak as lessm 4 1~ N%sC06 Pet 1. at I atm.
and 11-10 S. pet L at 6 also. Ca(011), WAns. alomb
00 ofishily tamer than XaX0# oclost., and = of Ca- goo
00 41 CO. abomb, I=" okwly of all, but we to use 00
b"Sumcfebeaptsm V01"thed.ollbeabourbintgoolas.
0* is inereassrd by the pessrom of law amts. of nitrate and goo
00 nitrite. the rate of aboorMian is lowered. Scrubl-, art
more dficinj for the xbawptkn than is bubblins the gas
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MONITION OV VYATIA ffAMMITS a WM06-
MMIC ACID A11) M PAVAWAIOS OF AMMORIC 4-# 1
i
ACID BY MCIPITATION WITH CALCIUM CARBONATE OR
11 VirkIz,, 3-.-XSr&bWp Wid I*
Nikonov (J. Chem. Ind. Rua&.* 1933, 10, Loss 7, 56-6' 2)
160 extraction of 11,P0,1 to obtained by usint surrillent
-10,0,.1' ECI to convert thl 95tire " preeent Into CsCl
20
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20--fiesh N
-!% is pptd. by C&(OH'; or Ca C03
from the solation 5btalrod after separatign from Insols,
notter (11) (asbout 26,9: of the wt. of (1) taken). (11)
settl** very slowlyp and is difficnItly separated by
filtrationj the product obtairsed bj pptn. of 1i PO
3 4
without previously eliminating (II) had IP 06 content
of 28%, as compared with 40% when (11) w:13 lbsent,
and only 70,5 of the P206 was assimilable. R. T.
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FERRLIUN,~ S. Le
Fiziologicheskiy analiz dar,-ykh lobeli~cvcy T,r(-,b.,r ,r4r 1 erl 4
21995 LFREL'M, S L
womonl knigooborota krovi. Vrachob. dolo, 1949, Vo. 7, stl,. 575-7e.
SO: LetopfLs' ZhurnalInykh Statey, tic). 29, Muskva, 1949,

JURBmt K.I.) MMIPAN, S.M.1 HMM, I.A.; IHAMAWV, 11,ke
hvpcwtional t-ray quantum counters aW their: use for X-ray
spectrta analysis, IsvAN SSSR,Sor,fls, 27 no,33,430437 Mr
163. (X-ray opeotroacopy) (KMA 16s2)

?~RONTN, V.T;.; F"TIN, Yu.P.; V"R~JJOVJ
Kly, B.T.; IVA!I(,,. ;~-T.; P-TPMAN, -1j'.;
I.h., KIIAIRLPYOV, V.A.; SITFLY(T, II.S.
Crystalles.-; X-ray spectrometer with stabilization of the
of the amn7_itude of the spectrum of a proportionil countjr. Zav.
Inb. 30 no.4:498-500 164. (MIRA 17:4'
1. KonEtru;l (far from the wall) Eq. (18) assumeep after some transforms-
tions, the form G(X);~'- to - hp(x). Prom this equation and Eq. (16)p the.
Beicond-kind Volterra integral equation is obtained for p(x);
S/170J61/004/004/0()7/014
Card 4/7

21776
S/170/61/004/004/007/014
The heat exchange in a ... B108/B209
P(X) M, (20)
h
6 (x) F (E)I, (21)
F (E) '. 3 e- dz, (22)
+ z +
wht!re is a dimensionless parametert
x (23).
13 , h Pe h
Pe is the Pecl.et numberp equaling the product of Reynold's and ran t1's
number. For not too great ~q Table I gives the values of the int6gral (22).
Fox great
Ca:-d 5/7

S/17 61/004/004/007/014
The heat exchaage in a ... B108%209
F GI) -Ir3 ~a, r(17 +
2r. 3 n+1 (24))
0 3
whitre a is determined from n (z)
(z)
n *' an z
(a. aI = -1, a2 - 0, a 3 1, The coefficient of local heat
exchange and the local Husselt number are given by
ks P(X) (25)
0 (X) ,
Nu, p (x) x, (25').
0 GO
The conditions for the validity of the solutions are 1) x/h~>1; 2)
50< Pe ~ < 2500. There are I table and 11 referencest 4 Soviet-bloc and
x
7 non-Soviet-bloo.
Card 6/7

21776
S/170/61/004/004/007/014
The heat exchange in a ... BIOB/B209
AMCIATIOR: Institut energetiki AN B~SR,g. Minsk
(Institute of Power Engineering AS BSSR, Minsk)
SUBMITTED: February 6, 1961
TWAut4a I
F (E) F (E) F (0 F (E)
0 1 OODO
1 0
5 5131
0
l
'O 0,4517 2.0 0.3921

0.1 0 6475 0 6
: 0 4887
:
i
.2
0.4367
2.5
0.38W
0.2 0,5896 0.7 0,4826 1.4 0.4229 3.0 0.3599
0,3 0.5564 0.8 0,4703 1,6 0 4115 4.0 O.i,193
0'.1 0,5301 0,9 0,4608 1.8 0:4025 0,0 0.971P
rable i
Card 7/7

C)/Y/
AUMM,
TITLE:
2 2,5': - I
S/170/61/CC~4/0-05/007/015
B100205
Perellmanv T. L.
Heat exchange in a laminar boundary layer floDing round
thin plates with internal riourcee of beat
PERIODICAL: Inzhenerno-fizicheskiy zhurnal, V. 4, no..t~, 1961, 54-61
TEXT: The syetem of equations describing the present problem (Fig- 1)
bread s
U_ + v 01
Ox 19~1) ay, ax TY
The, boundary conditions ar( c0 U (2). For the
u6_0 ' ly-O - 0, ly %82g/ay2
temperature of tle li4uid .-no finds QDO/ax + VaID/;Y -where
0 and are the boundary conditiono. The equPtion
OLO
=Cc
2t/a' 2 2
x
+ a t/ayj -Q(x,y,/k,, (5) holds for the plate. In these equa-
tions, t and 0 depote the temperatures of the plate and the liquid,
respectively. Ne author :orifines himself to a finite power of the heat.
Oard 1/ 4

22P2!,
S/'170/61/004/005/'007/015
Hett exchange in a laminar boundary... B104/B205
soiiroes (fq(X,Y)d.V