SCIENTIFIC ABSTRACT SLEZINGER, I.N. - SLEZNIKOV, G.I.
Document Type:
Collection:
Document Number (FOIA) /ESDN (CREST):
CIA-RDP86-00513R001651320010-2
Release Decision:
RIF
Original Classification:
S
Document Page Count:
100
Document Creation Date:
November 2, 2016
Document Release Date:
August 25, 2000
Sequence Number:
10
Case Number:
Publication Date:
December 31, 1967
Content Type:
SCIENTIFIC ABSTRACT
File:
Attachment | Size |
---|---|
CIA-RDP86-00513R001651320010-2.pdf | 2.57 MB |
Body:
USSR/Physics Nonlinear friction FD-1231
Card 1/1 Pub. 153-15/22
Author : Slezinger, I. N.
Title : Motion of a very simple mechanical system under the action of elastic
forces and nonlinear friction
Periodical : Zhur. tekh. fiz., 24, 166o-i676, Sep 1954
Abstract : Analyzes the second-order differential equation mx" 4 cx a af (x,,,t)
which expresses a system with one degree of freedom. Finds that this
type of motion depends not only in quantity but also in quality on the
parameters of the system (m,c), on the characteristics of friction and
the velocity of the slider. Finds his analysis valuable for machine
construction. Four references.
Institution :
Submitted : December 2, 1953
USSR/rEngineering - Shock absorbers
Card
'Authors
Title
Periodical
Abstract
Institution
Submitted
1/1 Pub. 128 - 2132
Erlikh, L. B. and Slezinger, 'Z.- N@
Shock absorbers
Vest. mash, 34/7, 5 9, JulY 1954
A report is presented on the theory of operation and function of shock-
absorbers. Oscillation calculations of.shock absorbers, are given.,to-
gether with a description of a shock absorber for-aircraft engin@ mountsi
designed by I. V. Analev. Six references. Illustrations; diagrams;
drawings.
...
SLEZITIGIM, I. N.
"On One Method of Solving Linear Boundary Value Problems of
the Self-Adjoint Type," by I. N. Slezinger, Odessa, Friklad-
nays, Matematika i Mekhanika, Vol 20, No 6, Nov/Dec 56, pp 704-
713 submitted for publication 4 Jun 55
The author presents a general method of solving a multidimensional
self-adjoint linear boundary differential problem, having boundary con-
ditions sufficiently general in nature, on the basis of the knou-n solu-
tion to the so-called "more rigid" X-oblem. corresponding tb that being
solved.
SLE- ZINGER I:N.
"On the Lateral Flexure of a Freely Supported Elliptical Plant,"
by T. N. Slezinger, Odessa, Inzhenernyy Sbornik, Vol 23, 1956,
Pp 105-110
This work presents a general solution to the problem of the flexure
of arn elliptical plate freely supported along its contour and under the
action of an arbitrary load which is symmetric relative to the major axis
,@f the elliyse. For the case of uniform pressure and load concentration
at the center, the solution is carried to final analytical formulas. The
solution is based on the use of a special orthonormalized system of bihar-
monic functions., which simplifies the derivation of higher order approxima-
tions and therefore permits the evaluation of the degree of accuracy of
the resultant solutions.
The article was submitted for publication in March 1954.
Sum 1219
SWINGER, I.N.; XRLIKH. L.B.
Designing smoothly moving feedmechanisms. Stan.i instr. 27 no.10:
26-29 0 '56. (K6U 9:12)
(Machine tools--Desigh-,-)
SLINZINGF,R,,,I.N..,,[Slezinher, I.N.] (Odesa)
Problem of the bending of a flexible recta-- kar plate [in
b. .
Ukrainian with summaries in Russian and ZnglisN - Pr3rkl. makh.
3 no.4:460-466 157. (MIRA 11:2)
l.Odeelkiy alaktrotekhnichniy institut zv'7azku.
(Elastic plates and shells)
SLEZINGER, I.N. (Odesa)
Castigliano's principle in the nonlinear theory of elasticity
[with summar3r in Nnglishl.' PrybUmekh. 5 no.1:38-44 '59.
(MIRA 12:6)
1.0des'kiy elaktrotekhnichnir institut zvlyazku.
(Blasticity)
S/04 62/000/005/032/072
.1UTHOR: C1 1 IYC333
L3i e zi n,_e
TITL!@. On v_riation theorems of non-linear elasticity
PERIODICAL: .11cferativnyy zhurnal, 11ate-matika, no. 5, 1962p 96,
ab@;traCt 5B432. ("Bul. Inst. politehn. Ja.@iil', 1959,
no. j-4, 83-86)
T---,*XT: The author gives the functional I(Um, K which
depends on the components of the displacement vector, the stress tensor
and t1to deforii-iations. The functional I has three summands: 1) volume
integral; 2) suri*ace integral which extends over that portion of the
surface where thu stresse@; are given; 3) Surface integral over that
oart of the @;urface where the displacements -are giveL It is shown:
I-L the v-riational principle'is complemented by the compatibility
conditions for the deformations, then the principle of stationary
-energy is obtained (Novozhilov, V. V., Teoriya uprugosti E Elastici'ty
theory] I M., 1958). By adding other'conditions the author obtains varicus
variational principles (by E. Reissner, K. Z. Galimov,.and others)...
[Abstracter's note: Complete translation.]
Card 1/1
ERLIKH, L.B.; SLEZINGER, I.N.
Designing mechanisms with screw pairs for fine intermittent feed.
Nauch.zap.Od.politekh.@nst. a4:18--26 159. (MIRA 14:3)
(Feed mechanisms)
SL.@,Zlll
Ali,-dicution of Ca3t-i@;l-janols principle in -0,01-,- 0:- -a:: ble
cl...3tic pL tes. 7 no. 1:(:@@-102
14:2)
1. Ocouskiy jjoj-.-urotc,.dmic:iusniy institut
(@,Iv,;;tic and shells)
30322
7 S/145/61/000/009/001/003
2 v b D221/D301
AiTHORS: Slezinger, I.N., Candidate of Technical Sciences,
D5-ccH.@E_,_an_J__Zr_rikh, L.B., Candidate of Technical
Scie-aces, Docent
Loss of stability of round zones on the surface
layer of machine components
PERIODME: Izvestiya vilsshikh ucbebP_ykh zavedeniy. Mashino-
stroyeniye, no. 9, 1961, 55-61
TEXT: The phenomenon of loss of surface stability differs
from that usually considered in engineering. The latter is related
to the deformation of the whole component, vihereas the fonner has a
local chaxacter. The close bond betvicen the surface layer and re-
maining mass of the body complicates the formation of the model for
iaveStIgati-i-C the phenor@.ienon. The author bases his simplified cal-
culation procedure on the significant stress gradient due to surface
loading.. An assumption is made -that in the considered elastic par-
tial spacc, the individual sections of a thin surface layer tend to
Card 1/4
30322 .
S/145/61/000/009/001/003
Loss of stability... D221/D301
def arm, and they have a circular shape and a symietrical def ormation.
Its QlOPIO-Ilt is SUbjCC-4- to tLIIO JE01101.7illg loads. Radial compressive
forces are dintributed on its sides owing to interaction with the
remaiuiro ', layer, TI-le radial, tangential aud norrial forces on the
lower base of ttv@ element follow the interaction @Ath the el-astic
partial s:,ace. The authors quote a creneral equation for the symmet-
rical def-orriation of circular plate attached to the solid base. The
aPprol:i-matc ct.-.lculation of the action due to the solid base on the
p-late is achicv&' with the use of single layer model- proposed by
V.Z. Vlasov aiid !".1N. Lcorttlycv (Ref. 1: Balki, plity i obolochIti
na upi-Licom osnovanii (Beams, Plates and Shells on an Elastic Base),
Fizraat,'Iri@-, 1,11@9 1960),1 This results in
DV14w + r(,,+,,) ' 21.1 i@,7, + yj., + P F
Tk
1- 1.7 It2 P 0 (5)
(0 T..7'(R) 0 (P LI ) .
R
which defines th,@ bou-vidza-y problerq. The approxirmate solutior, is
C ard -1/4,
30322
S/145Y61/000/009/001/003
Loss of stability... D221/D301
appearance to be evaluated. From the above, a conclusion is drawni
that the compressive load decreases with the depth fromthe surface
layer. On account of its rapid rate of reduction, an approximation
can be made ulhereby the actual state is replaced by the above meth-
od. ihe sLr'Lace- layer is often in a plastic condition, and thus
-the tange-intial modulus oE elzisticity should be used in the ex-pres-
sion of the cylindrical stiffness D. There are 1 figure and 4
references: 3 Soviet-'Dloc and I non-Soviet-bloc.
A3SCPCIATIONI: politeldinicheskiy institut. Elektrotelch-
i-a-stitut s-,ryazi- (Odessa Polytechnic Insti-
tut(,. _:Iactrotcchnical Institute of Communicatio-as)
C,ard 4/4
SLEZIIIGER, 1.14. [Slezinher, I.11.1 (Cdessa)
.1 @--- ---- - ,
Eonlinear plane deformation of elastic solids with a rectangular
cross section. Frykl.mekh. 8 no.3:330-336 162. (MIRA 15:6)
1. Odesskiy elektrotakhnicheskiy institut.
(Elastic solids)
IIATSIYEVSKIY, Anatoliy Gavrilovich; ERLIKH, Lazar' Boriso-vich; Prinimali
uchastlye: SIZZD-IGER, I.R., kand.tekhn.nauk, dots.; IIENAKER, L.S.r
inzh.; RABIT.MVl-C7H--,-T7F@.. inzh.,- SVIRIDETIKO, S.Kh., red.; ORLIKOV,
M.L.., dots., retsenzent; BYKOVSKIY, A.Lp i-nzh., red.;
GORNOSTAYFOLISKAYA, M.S., tekhn. red.
(Efficient organization of machipe-tool design] Ratsionalizatsiia
rasclietov pri konstrul-rovanil stankov, Pod red. S.Kh.Sviridenko.
Moskva, Vashgiz, 1962. 127 p. (MIRA l5t7)
(Machine tools-De sign)
SLFZINGERI I.N. [Slezinher, I.N.) (Odessa); BARSKAYA, S.Ya. [Bars'ka, S.IA.1
(Odessa)
Uonlinear plane deformation of an elastic space with a sealed-
in circular cylinder. Prykl. mekh. 10 no.3:31?-323 164.
(MIRA 1?-.6)
1. Odomolkly InfitItut, tilquzi.
RARSKAYA, S. Ya. [Barstira, S. IA.]; SLEZIIJGER, IeNo
Buckling of the surface 19-yer of a circular cylinderunder
strong axisymmetric heating. Dop. AN URSR no.6:7/+9-752163
(MIRA 17:7)
1. Odesskiy c-lektrotekhnicheskiy institut swfazi. Predstavleno
akademikom All UkrSSR G.E. Savinym (Savin, H.M.]
SLEZINGER, I.M., kand. tekhn. nauk, dotsent
Calculating nonlinear deformations of certaln pErts. Izv. vys.
ucheb. zav.; mashinostr. no.1:34-50 165. (14-TRA 18.1c)
BRESLAVP I.Z.; SLEZINGER, P.I.; FZLIDMAN, A.V.; KRUSHCREV, A.P.
Converters of phase-type control syBteaw of electric drives.
Elektrichestvo, no.7:48-53 JI 164. (MIRA l7zlI)
1. Novosibirskiy nauchno-issledovatellskiy elektrotekhnicheskiy
institut.
SrE, P. T.
Precision of t-e functional system of a program control of
a heavy-duty horizontal bori@g machine. Stan. i instr. 36
no. 12:15-19 D 165 (MIRA 19 -1)
SLEZ1NGER., S.I.; PROKOFIYEVA-BELIGOVSKAYA, A.A.
Succession of DNA replication in plots of large chromosomes in
man. Dokl. AN SSSR 161 no.2:459-462 Mr 165.
(MIRA 18:4)
1. Institut radiatsionnoy i fiziko-khimicheskoy biologii AN SSSR.
Submitted December 16, 1964o
PRCF,OF'lEVA-BFL'GCIISKAYA, A,A.; SLEZRIGM, S.,!,
DNA replication In homologous hiunar, IN SSSR
162 no-3,-681-68j, MY ?65. (KIRA 18:5)
1. Institut radiatsionnoy 1 khimicheskoy biologii AN SSSIR.
Submitt,ed December 16, 1964.
SLEZKIN, L. N. (Engineer)
"Effect of joints between channels in triaxial a o-stabilized
Ur
platform."
report present@d at the Scientific-technical Conference on Modern Gyroscope
Technology Ministry of Higher and Secondary Special Education RSFSR, held
at the Leningrad Institute of Precision Mechanics and Optics, 20-24
November 1962.
(Izv. vysshikh uchebny1di zavedenly. Priborostroyeniye, v. 6, no. 2. 1963)
- SLEZKIN, L. N. and KLINOV, D. M. (Candidate of Physical and Mathematical Sciences)
"Use of asymptotic methods in solving problems of the motion of an astatic
gyroscope in gymbol suspension"
report presented at the Scientific-technical Conference on Modern Gyroscope
Technology Ministry of Higher and Secondary Special Education RSFSR, held at
the Leningrad Institute of Precision Mechanics and Optics, 20-24 November 1962
(Izv. vysshikh uchebnykh zavedeniy. Priborostroyeniye, v. 6, no. 2, 1963)
h2539
S/020/62/147/001/007/022
B104/B102
AUTHORs Slezkin,
TITLEi Use of asymptotic methods for studying gyroscopic systems
PERIODICAL: Akademiya nauk SSSR. DokladYP 'v- 147v no. 1, 1962Y 57 59-
TEXTs The solution to system
+
ch ji),
has the form
a Sill 'P + eu, (aot, it.. pv) + r2tt., (it, tr, It.. JJJ (2)
+ a CIA# + EVA (a. t. q.. IQ + rhis (O"t. a., itit) +
where F_ is a small parameter, ui and vi axe-periodic functions of%# with the
a, are determined from
period 2Z; and oo It Ao
0
Card 116
use of asymptotic methods for...
S/020/62/147/00i/007/022i:
B104/BI02
can be derived, where
a Cos
(a Sint. - a cos T; -a cils it, - a sin a.'- a sin% N +
+ a C03
2A, ros it + 2B, a sin it +!!'l-I
I., +
A 011
+ - 2A,sint-2h,acost+'!! I-
(V (_ 141
_iAk a, - A,.-,int -till, cosir +
+ tug + ah V, - b&I -A, Jul -a, I)VI D, OU, _,I,, A, -!@6' as
4f r-r,. -w
&T, -Mn it A, )A, OA, #A
b, +@Z- ae 4- @ Z A
+ Cos it +,;A. + + 2,1,n,
-- 2A, 'Fill 2a a2l1l 2f Pd,
. not
Card 6
3/020/62/147/001/007/022
Use of asymptotic methods for... B1041B102
An analogous expression is arrived at for f 21" Fourier series repreeenta-
tions
fic, 9, (a. ft.) Ige. (not.. [I.) co% nit + h,. (ft. ft., 11.) sill ntl.
ji.) c0% lit + /1:. (0, ft., jQ.,in n*1'
(5)
(11. if., 11.) Cos fit. %III n*j,
AJ
+ cos nt I- tv@. (it. ft., %'lu ntol,
Card 4/6
Use of asymptotic methods for...
substituted in (4) yield
N -910.
+
a in!
nin- - 1)
S/020J62/147/00i/007/022:
B104/B102
(6)
In a similar way, higher-order approximations* can be reached. As an
example, a study is made of the equation of motion of a balanced gyroscope
with cardan suspension on an immobile support, assuming low frictiori in
the suspension axes. There is 1 figure.
ASSOCIATIONs Moskovskiy gosudarstvennyy universitet im. M. V. Lomonosova
(Moscow State University imeni M. V. Lomonosov)
PRESENTEDs May 25, 1962, by A. Yu. Ishlinskiy, Academician
Card 5/6
KLIMOV, D.M. (Moskva)! SLEZKIN,, %
___@ 'Moskva)
Application of asymptotic methods to the solution of problems on
the motion of an astatic gyroscope in gimbals. Izv.AN SSSR.-
Otd'.tekh.nauk.Mokh.i mashinostr. no.3:45-50 My-Je 163.
(MIRA 16:8)
(Gyroscope)
qy
AID N'r. 9)0
-6 14 Juno
SCIENTIFIC-TECHNICAL CONFERENCE ON MODERN GYROSCOPE TECH-
No@.OGY (USSR)
Izvestiya vysshikh uchebnykh zavedeniy. Priborostroyeniye, v. 6, no. 2, 1963..'
S/146/63/006/002/0101010
The Fourth Conference on Gyroscope Technology, sponsored by the Ministry
of Hi@her and Secondary Special Education RSFSR, was held at the Leningrad
Inszi,ute of Precision Mechanics and Optics fi?om 20 to 24 November 1962.
The conference was attended by representatives from 93 organizations in
i 30 S@: cities, including educational establishments, scientific research in-
stitu--s, design bureaus, and industrial concerns. The following are some
of the topics covered in the 92 papers present6d and discussed at the conference.
Vibrations of a gyroscope pendulum with a moVable suspension in a nonuniform
aravitational field: M. Z, Litvin-Sedoy, Senior Scientific Worker; improving
dynamic characteristics of some gyro instruments and devices: A. V. Reprikov,
Docent, Candidate of Technical Sciences; som@ problems of-the dynamics of a
I gyroscope with an electric drive installed in atymbol suspension: S. A.
Card -1/3
AiD Nr. 99o-6 14 ime
-N-UFIC-=CXTICAL COMMM.CE (Coat-dl
S
Cr- S/14,6/63/006/002/02-0/010
Rharlamov, Engineer; problems of the theory of the'inertial method for measur-
in- aircraft acceleration: I. I. Pomykayev, Docent, Candidate of Technical Sci-
ences; determining the drift of a floated-type integrating gyroscope without the
use of a dynamic stand: G. A. Slomyanskiy, Docent, Candidate of Technical
Sciences; natural damping of nutational vibrations of a gyroscope: U_Y__QaPALy,
Engineer; motion of a not quite symmetrical gyroscope pendulum with vertically
movable support: A. N. Borisova, Aspirant; gyroscope-type inclinometer for
surveying vertical freezing wells: V. A. Sinitayn, Candidate of Technical Sciences;
effect of joints between channels in triaxial gyro-stabilized platform: L. - N.
�kqzIcb@i, Engineer; theoretical proposal for the possible design of a gene;a@lized
gyro instrument: M. M. Bogdanovich, Docent. Candidate of Technical Sciences;
problem of drift in a power-type triaxial gyro stabilizer: V. N.' Karpov. Engineer;
methods of modeling random disturbances in gyro systems: S. S. Shishman. Senior
.@ngineer; method of noise functions for investigating a system subjected to random
Card 2/3
AID Hr. 590-6 14 Jime
SCM%'T1FIC-=-CMaCAL COM"EMICE (Cont'd] SI.146163100610021010103.0
S;g als: G. P. Molotk*ov, Docent, Candidate of Technical Sciences; drifts in a gyro-
stapilized platform as a result of the effect of cross joints un'der determined and ran-,
dom disturbances: B. 1, Nazarov, Docent, Candidate of Technical Sciences; stability,
anq natural oscillations In inhomogeneously rigid gyro systems with backlash under
extiernal influences: S. A. Chernikov; methods of designing a gyro vertical with.
automatic latitude and course corrections: A. V. Til', Candidate of Technical Scien-
ces-, use of asymptotic methods In solving problems of the motion of an astatic
gyroscope in gymbol suspension: D. M. Klimov, Candidate of Physical and Mathe-
ma@ical Sciences, and L. N. �Iczkin; theory of aperiodic gyro pendula: V. S.
Mlochalin, Docent, Candidate of Technical Sciences-, and selecting basic parameters
of course gyros py uting nomograms: V. P. Demidenko, Engineer. [AS)
Card 3/3
L IP16-63 EW(d)/BDS--AEDC/AMO/AFMX/A.PGO/ASD/SSD--pg
-4/Fk-4/PI-4/.
Po-4/Pq-4--BC
ACCESSION NR: AP3003453 0045/0050,
S/0179/63/000/003/
AUTHOR: Klimov) D. M. (Moscow); Slezkin, L. V (Mosecrit)
of problems concerning,
TITIE: Application of a.symptotic methods.to thesolution
the motion of an astatic gyroscope in gimbal suspension
SOURCE: AN SSSR. Izv. otdel. tekhn. nauk. Mekhanika i mashinostroyeniye,.no-
1963, 45-50
TOPIC TAGS-. application of asyzptotic methods, solution of differential equations,:
gyroscope motion
ABSTRACT: A mechanical system described by the =nlinear differential equations
given in the Enclosure has been studied. The equations are solved by the
Bogolyubov-Mitropollskiy a--Vmptotic method for a case in which thecharacteristic
determinant of a nonperturbed system has two conjugate pure imaginary roots and
two zero roots with linear elementary divisors. Solutions x and y are determined
as series in powers of a small parameter for the nonresonance case. A method is
Card 1/3
L 10316-63
ACCESSION NR: AP3003453
described for obtaining first-approximation equations, on the.,basis of which
solutions of the system of differential equations axe obtained. Byanalogous
procedurd,, equations of higher approximations can be derived and solutions by
corresponding approximations established. 'As an example, the notion of en
astatic gyroscope in a gimbal (Cardan) suspension with dynamically unbalanced
rotor is studied, with small dry and viscous frictions of the gimbal axes taken
into account. The system of second-order.differer-tial equations describing such
a motion is written in a dimensionless.form and then, after certain
transformations, reduced to a system of equations similar to those given in the
Enclosure. On the basis of the system offirst-apliroximation equations,
pecularities of gyroscope motion are analyzed. Orig. art. has: 20 fo,-nmlas.
ASSOCIATION: none
suBmiTm: oiFeb63 DATE AoQ: 24ju163 ENCL: 01
SUB CODE: 00 NO IW'SOV: 003 OTBER: 000
Card 2/3
ACCESSION NR: AP4043899 9/0179/64/000/004/0146/0147
AUTHOR: Slezkin, L. N. (MOSCOV)
TITLE: The effect of inertia of Cardan suspension disks on the motion of a gpvscopic
integrator of linear accelerationA
SOURCE: AN SSSR. Izvestiya. Mekhaniks. I mashinostroyenlye, no. 4, 1964, 145-147
TOPIC TAGS: gyroscope, gyroscopic Integrator, linear ameleration integrator.
gyroscope disk inertia, Cardan suspension
ABSTRACT: An unbalanced gyroscope In a Cardan suspension Is used as the sensitive
element in instruments designed for measuring the apparent velocity of mc ving objects
(A. Yu. IBhlinskly). The angular velocity of the external disk of such a gyroscope Is
given by
da Mgt
1-
"@cording to the precession theory. This equation is very accurate for existing
gyroscopes when the gyroscope has self-excited oscillations with a low amplittide and
high frequency actually coinciding with the natural frequency of the instrument. In some
time
cases, the self-excited oscillations are replaced by a conservative system. A
C:Card 1/3
ACCESSION NR: AP4043899
drift of the gyroscope appears when the disks of the Cardan suspension are not parallel
and there are mutation oscillations (K. Magnus). This was analyzed in the paper by
D. M. lGimov. The cause Is the Inertia of the Cardan suspension disks. The equation
for motion of a heavy gyroscope in a Cardan suspension is:
(As + Ct (A +'Al - Cj) too' 01 a' - (A + Hi - Cs) all'sin V - 8 coo W ses q
(2)
H " C ty - 4, sin 0) - const
In a gyroscopic integrator, the plane of the Inner disk, determined by the axes of
rotation of the inner disk and rotor, is almost perpendicular to the axis of rotation of the
outer disk, while the turning angle of the inner disk relative to the outer one to small.
Therefore, for exleting InstnLinents:
(3)
+ + 20.@) + 2 (e + + 6) 1 - Aa* ell 0.2 + 1/6 62 + %5)
+ e (x /A) (e + b)'(P. + 6) +(1/1 All + 11,62 + 0.6)
(A DT-G
Cold 2/3.
ACCESSION NR: AP4043899
On the basis of equations evolved in the article it is concluded that the motion of the
gyroscopic integrator along one of the axes may approximately be taken an consisting
of three motions: precession at constant velocity, oscillations with circular frequency
superimposed on the precession, and additional motion. The additional motion leads
to errors In Instrument readings. no relative error of the instrument In expressed as
follows:
IIIII (A, + GJ 0. an (A 4@ D, SA + 04
(4)
2 (A. + A @+D s) WA - -A-;T-;i
Orig. art. has: 14 equations and 1 figure.
ASSOCIATION: none
SUBMITTED: 18AprG4 ENCL: 00
SUB CODE: NG NO REF SOV: 004 OTHER: 001
Card 3/3
1, 2943-66-- EWT(d-)/*FSS-6-2/EEC(k)-2/EED-2/EWM-c-)--X-..-.-,.-
:ACCESSION NR; AP5021444 UR/0146/65/008/004/0065/0
531.383
01-7
'AUTHOR: Slezkin, L. N.; Wang, Tan-chih
':TITLE: Effect of coupling between gyroscopic platform channels
SOURCE: IVUZ. Priborostroyeniye, v. 8, no. 4, 1965, 85-90
,TOPIC TAGS: gyros-ope motion equation, motion stabil
ity
ABSTRACT: Linear coupling between gyroscopic platform channels may be due to the
moments of,vis*cous friction in the axes of precession of the gyroscope units, or to'-
the fact that the angle-data transmitters for j-
-the angles of precession fix only the..'
relative rotation of the platform and the gyroscope unit. The authors study the ef
fect of these two factors on the stability of several types of gyrostabilizers. It!!
is assumed for simplicity that the angles of deviation of the platform relative
0- i
the inertial coordinate system, and the angles of rotation of the gyroscope units ain-
i-small, and that terms 0
f the second order of smallness may be disregarded.. Th
tem is assumed to be made up of absolutely rigid elements. Tha.parameters of the:@
[;ard
L 2943-66--,-
ACCESSION NR: AP5021444
channels of the platform are assumed to be equal.. A system of motion equations is-1:,:.
given for the triaxial platform shown-in fig. 1 of the Enclosure on a stationary I:-
base. This system of equations cannot be analyzed,into three independent subsystem
A block diagram is given which corresponds to this system of motion equations., The-.-
coupling between channels is shown on this diagram. The cross-coninections due to
the two factors given above cause motion withjespect to all angular coordinates...'
when there is a moment of disturbance with respect to one.of the axes ofthe stabi-@
lizer. These linear connections are eliminatdd by using-paired gyroscopes.' Orig.
art. has: 3 figures, 14 formiulas.
ASSOCIATION: Moskovskiy gosudarstvennyy universitet im. M.,V..Lamonodova (Hoscow-
State University) qLA
SUBMITTED: 26May64 @ENCL: 01 SUB CODE: HE
NO REIF SOV: 004 OTHER: 001
Card 2/3
L 2943-r66..,,-------,-----.
ACCESSION HR: AP5021444
SIS"'KIN, N.A.
Boundary layer near a plate in a flow with jet separation. Vest.
I mekh. 19 no-5:67-78 S-0 164.
Mosk. un. Ser. 1: 1-!at.y
(14IPJi 17:12)
1. Kafedra gidromekhaniki Moskovskogo universiteta.
0 0 0 0 0 0 0 * 0 0 0 0 @ 0 0 0 W-w- V
0 . V"O
94404100004111000000@-of
1 4 to 0
1 3 A 1 6 1 1 # IQ 1, it I) m is Ily Is 1, a Pia AWA )4 fix it 11 Ij is It
A III JL.A-Z, Jt- 1--A- L a m 66 @k M (I
o." I
00
-00
se
&rowA a curve-Amptid obittructim. N. A. Sk-Aia-;
p. Prod. acad. irri. U. R. S. S. 2, 512-50%15)(in
man 515). -The Caplygin approtimation method is
rided to the cam of a curved rigid boundary. The
% (If 1xvi-Civita and Villat are redur'A to an inirgro.
rrntial "jumtkni. As an exaltildc the titivicning of a
around an object of circular cro". section wa@ inv"ti-
The c%istence nf a solution can 1,e %hown by
ted
method -If sticcc,@Ayr approximation%, anti the uilution
If (Imirit %I Fvam COO
s
..I
e
0
00
@00
-,so
zoo
rooots,
0
0'
018
::oe
*0
Jib t
.00
WOO
IL 7;;
` ;0
A An L 1 4 OW 0 W 1. TW.' -- 0
to It TV C4 "In n 1 -4 &MO
0 0 si
i 9 0- 0 st 0 o 0 0*4 too. 0 0 0;0 006 so o 0 0 0 0 of 0
voL@ru";- C. s o,.
7:
f
14 sh.
idtuil:@, Froi-derri of t'lle bro-di:-Ie.-isional Flow, o' -:as.
1480'8 1937, no. 7
So. Sci, lice --L;,i(j Aviqtion in @Ahe Oovis:;t Union. Librar@@ of
Go!l:-rp-s.s,
1
'l' iarr .. U@j i v@- ---s 1 te t.
-zc @yk . %--oInaskh. (@,@Osco;.-.
C,b
11 -piski, 1937, no. 7: Mekhariika, D. 71-132)
--r-,,-nye za
Sun::iarv in Enrlish.
Tit--'(-@ tr.: un s-,rady capillary :,;aves.
il)60. ,"4,868 1@37, no. 7
,"eronw,itacal .-;cience and A-liition la the SoVief, U!il,(-)n. Litwary of
conc@ress, 1955.
v tzJ1 iidra v zhid@ onti. 0-'Os ow.
"I K
!-'et. Ucheny'." 1-1,4:0, no. 146: @Iekhaniika, P. 12-37)
Ti-tir, tr. : fjnsl@-.eady m(Aion ci a cylind,-.- -In -a vjscou3 fluid.
Oa. m.868 l9bo, no. 46
!@O. I.PronauluicRl- Science and AvJntion in th,@ -"ovi-et Union. Library of
t7
-LE,
'.7br., 2-1,111-x7 Cr-ler L,3,-lin -- Orler :5rva--ov F. Z. D--exm"h!ns,*
-nr- of Proi.@@7-, -`OtatLon of a -':@rojjctile," Dok. 30, lio.
117eM@-11---ation o ThLi -Flaue Lyto a 71. :-cous I., :1@6 -.'o I I a 16 -
IIC,n t-hj o--" .'aftnim, the Sol-ationz; a-f -"quations,11 ilbid., 54, Eo. 2,
1@46; "On L-tie 'Zollin.- of a Cyll-nder ove-r -- --'@Urfacc Covarad ,.rith a Viscous Layer,
'i lidi-, -.0. 3, 1946;
i 0i' --;0. 7, 1946; "The --@@ueralizeld Equations of ?Lay-riolc'ts," :LO a
IlThe Distr;-biAion @@AVD---@inatioiri of Pnsair-- on thc -urface of a Eilattemd cilyas
0 4 0 9 0 & 0 0 a
6 a 0 0 0 0 0 0 a 0 0 0
0 U It Is 11 to a u a id a b v x $I -a- a
A t L A ".-f. L-L-A-9--f 4 1 1 1 U I 117-Ja In AJAI SM #--A
-00
cow a amew" *a
A. CA Amd. sd- VA&T-
-00
~q"WO;2A-dWWgr Cy*W" of O-n
00 7) -06
an ft borbow Oaft
0 abm^ t:O'jWW#M= Jsc@y. A ft--k 000
"efed brim is siod ad all -pMm'- f- dw moo
for ths cra" we r. It 0.
oil; cOO&k"4(rd"j'--1 babuMmL t 00
000
533.&SI 1.5 mo Abw. 20
moo
00
r
0 rSOO
800
go*
00 400
.011
moo
'00
moo
'00
'00
wo
V*. let. goo
PWAL
L
W-Wh u a 99 a 09 it x 11 1 sa a 0 0 11 Ir so 0 a 1 .3 0 T
It KO 1 0
]@Lo :-e 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0
a +00
-,09000*0000000000000**00000000000000poo
W-1
lo
v a 4 1 A, r -M It CC U
Al
A
v me @k
fl A 0
r U.Wkiata Mution tA aC fillder ms a Plalle SlAyffl, V U-v
ki ervel with a IA)cr uf Viscous Sub%tarkv. N A. Nle4llL
00
Zoo
Wl 4ITALkIJRGK4t illIkATLONI CkAMMATICh
ros,
ir'
It It An A I IW 0 a
. . - - I lu
as *0 0 0 0 *a*** 6 6 0 4 gas W11- I- t-q- 0--m -a-
a 00 0 4 0 0 OW,
- no -. I
w is I& v w x
a
A@C 2 OL - j- r...li-v 90-
00 .V@ GeV!?% V..Cmof *I
04.10,40141 .01.
SA A53
:a 00 lb womm d ed C.AL *.L Sd. UNSS. 94
T4
in a layw of .00
(No 2) 21-t@. 00* MX'00
a ;;@ - - i @ ft - ie COWWWO& Mw C-0 A*
dalbu, "d fivw tbew
my be
t-lowledot0imofurimbut :
from thwakdovem COW* bA vadMim OfP*mm
the vbco@W
akme tbt *A*@ of the byer am zoo
he w"SwWw. A ID
10
its
og'
10
6 -00
00
114i
S I &CTALLUIRGKAL LITFMAIL,41 CLASSIMATICU C-2-
Is
lopt t4mo.o ;7-T- SIIQ.@ .11 @. get 48
0
u it ky -0 Ls L w 0
qr9-Kr-lrc-7aT It Kw Kww wt 114
a 0,0 0 0 a a 0 a a 9 a 0 0 0 0 * : ;
0 0 Is 0 0 0 a 0 0 0 0 0 a 0 0-,
9 0,0 0-0-0-0 0 0 0 0 0 0 * 0 0 o,1 0 : *10 0 9 0 0 0 0 a 0 0 * 0 0 **see
0040 0 0 o e # a 0 *go* (- * . .' - * -. -11 -
t. 099 iO09000040060060 -
0 1 j 1 4 1 -A I I f V it U a w is M 11 V it a a 30 H 33 a 34
A A a L Ak N F a I I AA N IR A.- -
W AMD 1.0 toot*%
PIC-CISMS AND "CrI41111 .09.
/
arA
1102. GEMILT ZED IQUUTIONS CF RgrNOLDS- SleskIn,-fi. A. L
Targ, S. M. (Compt. Rend. Acad. Sol. tI.R.S.S., 1946-sU; 205).
The approximate solutions of the equations of Reynolds, them of
001, , using the method of Wbenson,
lubrication can be made more exact
00 A
' ,
by taking into acco=t the quadratIc Inertia term, on the basis 9f
001 2, 1
01, Prandtl's equations. Frandtl$# equations he" now boon nod1fied by
a partial averaging method to give now equations uhich are also app-
0*0 '! 1
;:
licable to problems previously studied only by Reynolds' equations.
006 ;
fl--
, -
i
The application of the new expressions to some particular problems,
og -
t ncluding tlow post a plane plate, is briefly discused.
a
804
z!
I "A
ANTALUM61CAL LITIMAIWE CLAINFICAIM
it 141040 jilt a" off "1171601 814121 40 a" 191
U S AV 03 - I f I - 11 AR L I a ft & 0 1 V N I do 0. .10 T
a a it a a it It 'a 'a' At
A
0Is 0 10 0 0 0 0 0 0 0 0 9 0 0 0 it 00 -00 0 0
0 0 0:0-0, S'Av 0-4 * of, 0
10 0
We 0 0 0 al 0 0 0 o 0 0 0 o 0 0 4 * 0 0 C.40 006600*4060600-0
,-,*Joe*** $Goo* of $*Go
0 0 0 0 0 6 a 4
L6 it is lentil a n u2i jivab-.1011 12 u )A 31 1$ v If It 1 41 Al #I
toA r I ALAHLOC
04 53L51: 334.2nl
47L Us do
06
do 61 omiam it a dML SLAWAR, N, A.
C-R- Acak Sd- UASS. SO (W 7) 1.
F--A.-Rcya"'mqmmkw m wrkft dmn MW
00 SWVW ror a two byw h - on owfam of the sw
0 -A thc suff&x of tM tibock WOL Fmm &,, m
0 Jr! oquadmit, of %owe mv. b A- I" the prmum
&W fonnvb for dw fb&W in ten
0
0( &Nkq fuwtiom of** wood him& L S. 0. zoo
so 1i
ZOO
00
of
00
00
&S-SIA sfTALLUPG1C4LL1TCW.TL4f CLASSIFICATIG@ 9-2
411111 -30 a@v
:.f .11,11 41% Le 0
-*j--&-P--F@-'j I AR I I I OW 0 Pi 0 If IN 0 A 4 3
A,
it el
0 0 0 0 10 0 09 lp of 0 of 0 0 0 0 0
SLEZKI'r, . 12
tl
71,
ye
ca-.-Aliari wnv,,,,@-
146-08 15)3Y, rio. 7
@cj,@!,,ce nd Avi;ii.ion in tno "ov@-4. Union. LiLr:@rIv 0,
SLFZKIN, N. A.
Fluid Dynarrics
Level flow of an ideal fluid around a gas-filled envelope.
Uch. zap. Mosk. un., No. 1, 1951.
9. Monthly List of Russian Accessions, Library of Congress, May 1952. UNCIASSIFIED.
see 4 0 '00
4.@ 1; .1 . It
0 it 17 a IV 40
16 It 14 24 Is a k.1
a 10 it it 11 M 11a -1 M
o
Ir c, i -fD c-pto,
7076
ON THE DIFFERENTIAL KWATIONS OF GAS MOTION.
04 N.A-.Jle&IU!!. Doklady Akad. Malik S.S.S.R. 77.2. 205-08(195lj -00
Mar. (In Russian)
0 An abstract appears In Applied Madwinics Rove. 4, 567 .06
119 5 1) Oct. and is reproduced here in part.
The equations of cowleutty, motion, &ad energy are
'Written in ardiogonal curvilinear Coordinates differing from -00
00 the usual form by the addition of terms representing dif- 4 0
0 fusion and thermoddiuston. '00
00
0* S,
eg
.00
0 p 0
'00
-00
1-00
tz"
jIgnAtual CLAS$IPKITIOO 0.0. too
0 ETALLuPOICAL L - - --- - ii -ii-
11), 0@' LI,
61111, 01" 5 A3 a 6 1
0 t It It it 01
so 00
00 0 9
00
0 ago
0 0 di 0 0 0 0
SLE-ZKIN,. N. A.
LISSR/Geophysics - Filtration 11 Aug 51
"Differential Equations of Filtration," N. A. Slez-
kin; Moscow State U imeni M. V. Lomonosov
"Dok Ak Nauk SSSR" Vol LXXIX, No 5Y PP 755-758
Attempts a new derivation of the familiar eqs de-
scribing the motion of a fluid in a porous medium,
thus leading up to the ]problem of the deformations
of ground under the action of filtration flow. Pre-
vious setting up of these'eqs employed assumptions
that the ground is immobile and the porosity is
const. SuIbmitted by Acad A. I. Nekrasov 16 Jun 51.
21OT44
Mathematical Reviews
Vol. 15 No. 3
March 1954
Mechanics
jWaWj..N. A. The differentw equadons of the AWfMTn&.
uk-55S
MkIady Akad. Naw R (N.S.) 00,'
561-564 (1951). (Russian)
Obtekardhi rmpo'@nfmnoi o!-)o1octj'Vi ploskim potokout ideal Inoi zhidkosti. (1-losrow.
Universitet. Uc:@Ieriye zapiski, no, 152: I'clainnika, v. 111, p. "1-715'
'1-,'tle tr. :Pl,-jne flow of an ideal fluid around a r7a---filled shell.
Reviewed by J. V. 'iiehausen in ILathematical Reviews, 1953, v. 111, no. 5, P. 508
Q60.1,1868 19511, no. 152
'10: @eronautical Sciences and Aviation in the Soviet Union, Lihrary of Congress,
1955
USORNthavatics - Osseo" Flow ftr/Apr@ 52
-116&ct 'of Fiat . aw"W" ftweam -on a Bousalass Wall,"
I. A. Sleakino ftecow
"Prik Natemst i Nekh" Vol XVI, So 2, pp 227-230
Sleskin uses S. A. Chap lygin's method (cf. "Gaseous
710W" 1933, VQ1 II) to solve problem of iWact of
poems stream against flat wall, providing vel-
ocity of stream in inf inity isf perpendicular to
wall. Partial soln of this problem vas also given
by 1. To. Zhukovsk:Ly (cf. "Modification of Kirch-
hoff I a Law" 1936, vol iii) and by W - Schach (of.
2o9T68
USSR*thematics Gaseous Flov (Contd) Mar/Apr 52
"Unlenkung eines freien FAIssigkeitastrahles an
einer ebenen Platte" 1934, Vol V). Received
22 Mar 51.
209T68
SLEZYIN, N. A.
Evanoration
Principles of the I%vclrodyna-mic theory of evaT@ora-
tion off moisture by wind. Dok-1. JQ11 SSSR 63, ITO. 1,
1952 Moskovskiy Gosuderstvannyy Universitet im.
M. V. Lomonosove. Recd. 28 Dec. 1951.
SO: Month List of Russian Accessions, Library of Congress, August 1952 ip)5y. Uncl.
SLEZKIN, N. A.
USSR/Physics Hydrodynamics 11 Sep 52
"Differential Equations of Motion of Pulp," N. A.
Slezkin
I'Dok Ak Nauk SSSR" Vol 86, No 2, pp 235-237
Mechanism of transfer of ground particles by water
is similar to that of transfer of water particles
or oil by gas in airlifts. Shows that in the sub-
ject case of transfer of pulp the eq of motion
separates into 2 independent eqs describing the
transfer of the mass of each component of.the mixt.
Submitted by-Acad A. I. Nekrasov 5 Jul 52.
235T95
2-35T95
czKtn, V. A. Ueneralization of Helmholtz's theorem ori
X,
I-htliernatical Reviews. the resolution of the motion of a particle. Doklady Akad.
Vol. 14 No. 8 Nauk SSSR (N.S.) 86,477-480 (1952). (Russian)
@@
Sept.1953 The author points out an analogy betweell motions of .1
Mochartios. physical systvin composed of discrete particles and I lelin-
holtz's theorem for liquid motion. Ile sets up differencet
qtiotients.,tti,ilogotistocotiipr,tictitsof vorLicityanddeforma-:
tion rate for a tetrad of points, and studies changes that:
come about due to translations, rotations, and stretchings.,
lie indicates that these operations can describe the transi-
tion from the liquid to the discrete system. The discussion
is chtirely theoretical, with no illustrations or exampIles.
R. E. Gaskell (Seattle, lVash.).
6' - ro
USSR/Physics - Hydrodymamics Sep 53
"Generalization of the Helmholtz Theorem-.on the
Resolution of-the Motion of a Particle,'i".J.Prof
N. A. Slezkinj;@Chalr of Hydromechanics
Vest Mos Univ., Ser Fizikomat i Yest Nauk, No 6)
pp 17-33
Continuation of his article (Vest MU, No 10, 1951)
in which the author established the differential
eqs of motion of a deformable medium of particles
with variable mass as an eq of macroscopic transfer
of mass, momentum and total energy, Discusses ,
275T98
here: the relation of He imholtz's theorem to the
theorems on the 'Linite displacements of an abso-
lutely solid body; Helmholtz's theorem for a dis-
crete system of points, and generalization; the
variability of the mass of a particle; the method
of averaging;' the dimensions of a macroscopic par-
ticle.
ST-W-KIN, IT.A.
Generalization of Helmholtz's theorems on the analysis of particle dynamics.
Vest.Mosk.un.8 no.9:17-33 S 153. (MLRA 6:11)
1. Kafedra gidromekhaniki. (Dynamics of a particle)
-SLEMINY
USSR/ Aeronautics Fluid t4echanics
Card
Autbors Slezkin, N. A., and Shustov, S. N.
Title Stability of motion of a particle suspended in a laminar.y flow
Periodical Dokl. AN S35R, 96, Ed. 5, 933 936, June 1954
Abstract The 'Stability of motion of a'particle suspended in a laminary now @n. s
investiCated with consideration of a lateral force proportional to the
density, circulation and relative rate of flow around the particle. The
necessity of considering the lateral force during the study of the Mo.-;
tion of a particlain a laminary.flow is dictated not only by the results:....
of numerous investigations clearly showing the formation of a lateral,
force as result of a circulatory flow or as result of the presence of a
natural body of rotation, but also by the fact that the formation of the
very circulation in the flow is due to the viscosity effect of the li-
quid. Three references.
Institution The F. E. Dzerzhinskiy Artillery AcSdemy
Presented by Academician, A. I. Nekrasov, March 11, 1954
24@'
IA1499. Mukja'gj@'a' Dynamics of Viscous incompre@Ale'
fluid ifesz.hicasemoi thidkostil, Most
Isdat.TAh.-Teor. Lit,, 1955j,51.911P. 10'r. 90 1-
This attralive work'oriOnates in tile authors lecttftes at the
nwwl 1-inathematitall -faculLy -of, Lba Nfo---ow University. It.
ttim . A tuXUMk fOrAlIC StUdants of hydrtalyntunies at
is "rr
Russian universities.
in tile saim of lite modem killotiv theory of fluids, the book
emphasizes, on the one hand, tile connec tion and analogies bL,
-dy
tween the nuna a of a viscoun liquid and, on the otherthe tit-
vLlopniwit of the theory of elastic deformations in sidids.
Citusiden-d am problems tractable by means of inwhanical
xonerptiorm only; questions concerning the comprMibility and i
heat Conductivity of liquids cannot he trtated in bdokg of, tills
kind. Problems illustratinj t thL omtical cowdderations are carc-
fully work-in), l~giiiiiingwitli~t)lu*rn~itilellt..Itirophysicalforinulll-.
tion and up to a delailed aludyllis of tile final solution. 81xvial
attelition is Iliad it) explai3anK Various niethods for Amplifying
tile fundiunental (4juntiotoi, of motion inoirder to make , them
approxillinfo, gniatioll.
Thebook ollell" with.an exteiwive infroduction rot keerning, Elie
hilit'llill'a) devVION"It"t of 113-d"AlMloat-21. Thi! It"111111 lextis
Oividt.d fillo 12 rhall!e1v 1@itjx 07 8 and fill, Volume
l
anal indvx, rollowtit liv it. dt@
calls with it nither complelitt- nou
tailt.41 list fif inatteN triwivi. There arv to!) instrudive figurva
thsaigliouttlielext.
edge in solving partial diffemitial problvinK hY t-latisival lutthod.-I
11.4 well its Ily Invull3of the Laplave traAwforswithlit.
TIM (011AWilig he3diflgl; Of Wparato rhapters will give a more
"net idea of the content. 1. M-formation voloviticA of a p!srticlo.
C, mponents of 8treas. 11 Diffilrential equations of Illation of a
viwc-olul liquid. 111. General properties of motion of viscous
fluids. IV. caws of ilitegmting e.-mutly the differential equa-
tions of steady mat ion a f viscous liquida -.V Mation of a viscom
fluid for small Reynolds numbers. I'he Stakes method. VI.
Hydrodynamic th(,ory of lubrivations. V1 L Motion of a viscous
liquid for small Reynolds numbers. Tho Oficen method. VIII.
Theory of boundary layers. Ix. Unsteady motion of a vlwous
incompressible fluid, X. Development of the lan-winar motion of
liquids. XI.SLaijilityo~taftiiii!Lrilow~. -XII.Turbulentmotion.
Presentation is clear and vivid, papor good, and print legible.
Only a lot of unneecswy misprints and typographical oversights
considerably disturb the baullmhud -enjoyment of reading
this wictilific wurli-. 711tviewer wiirntly revonaneuds the book
not only to spetialists in the liwld of hydrodynamics but Also to
applied niathetnaLiciaus and phyeitii4tq.
V. vulli6ka"Czechuslovakim
SLKZKIN, R.A.
Flow of viscous liquid with a porous bottom as free boundary.
Vest. Moak. un. Ser. mat., mekh., astron., fiz. khim., 12 no.5:
3-5 '57. (MIRA 11:9)
1.Kafedra gidromekhaniki Moskovskogo gosudarstvennogo universiteta.
(Fluid d7namics)
AUTHOR-: SLEZ.KIN, N.A.. (Moscow) 40-4-22/24
TITLE: On the Flow of a Viscous Liquid Between Porous Parallel Walls
(0 razvitii techeniya vyazkoy zhidkosti nezhdu parallellnymi
poristymi stenkami).
PERIODICAL: Prikladnaya Mat..i Mekh.., -1957!, Vol-.21., Nr 4-, PR-591-593 (USSR)
ABSTRACT: Stimulated by investigations of the boundary layer in which
the walls are presupposed to be porous (see Wuest, Ing. Arch.
23,3-,1955-) the author considers the Course of the flow of a
viscous, incompressible liquid between two parallel porous
walls in the stationaryg plane case. Under partial con-
sideration of acceleration and viscosity there hold the
approximative equations
2u
U 2u 1 a 9 lu
--p- - 0 + 0
3x 3x 3Y2 9y - @x @y
with corresponding boundary conditions (U is the medium
velocity in the cross section). With the aid of the Laplace
transformation the author obtains rather complicated solutions
for u and p-p C (PC the external pressure, constant), fur-
thermore a condition under which the pressure in the channel
CARD 1/2
On the Flow of a Viscous Liquid Between Porous Parallel Walls 40-4-2@/24
only decreases.
SUBMITTED: March 19, 1957
AVAILABLE: Library of Congress
CARD 2/2
AUTHORSe skoryy, I.A.. Univer.1ty Lecturer, and S07/555-58-2-33/35
10 PytOv# V.D., Scientific Assistant
TITLE, Loctonotov - Lacturea 1957 at the Lech%ntc&l---'athe@-Iz&l
,&Cully 0fMancov State University (Lomono-ovskiya
."Ohiya 1957 god& na zekhaniko-ateratichaskon, fakullt*te
MOU)
PERIODICALi Voetnik Lesko' :kogo Univoraitotv. S-.4:4 mat.-tW, wckh-aiXI,
"troDomil, ti ixi, kh1mt1, 1958 .tr ,pp 241-246 (unR)
AJSTRACTs The Lomanomov lecturas 1957 took place fro. October 17 -
0 -th anniversary
, 1117 and warcddlcsted the 40
,
Iol t
:r
.;
o
,,
. br r v.I.1ion.
.
In tb. ..Ir:l m:eti na IN. 901mogarov, Academician spoke
Go Approxiouttive Representation of Functions of Several
Variables by Superposition o! Functlans With Less Tariablo.
ction".
&C4 6
lla
*,
Pu.
In
of
Th.
I
*ctur. generalize.
ropf of
;
,
l
.
V
,
,he re ul . Of ir . :r., A 0. It shk n, . . Arnolld and
t
,
,
,
T.N. Tithozirov. The content. has been already published
(Doklady Akadomii nauk 55SH014.5). Professor
2-_ %embor of
-hs
d4XY of
Sti.=*. Of the U%. SSR,. *PQkG-OT1
&,L
_-
,
-
.
",
*all, ,on o@ the Boundary Layer of the Moticr, or a two-
'
:
Gopon.. t
Ll 'u id .
Th, OtbIr lectures war, 91-n --parately in the sections
Mulchani 6 and mathemati.
_.. I.n. jol]owjC4 I-tue. were given.
:
1. ro
P f
osor L.N. Sr#14n*kiy, Corrosponling Lecher, AS USSR
Propagation Of SoCnd We,.. From
- Rotating Deformed 3,11.
2. Professor G.G. E@trcyy;
The Flow Aroun:i Thin T@ncatqd
Gas rith Sigh SuP-tfion'
,i Velocity.
y
S
N Nikifor Properties of it.. C.icu,.
3. Prof o' '
-tion,
COAstruc ic r.
tad '@@4`u Of EXdzo'*-hnt@%I rxks. on the
Rivers of the Central Strip of th.
4. Prof*aaor A.ya. E-92- nY-n - P-n.tr4tiin of a Rigid body
Into the Ground.
1. M.Z Litvinov-S*doy, So
ni@r 5@1.nttfj@ Ascist-mt 1 0. the
6To t a C rt4its With 3.uni.d jrt.rv%l of
Sni" Is Of 1, r I
I
aristion of the Controlled V.rl.bl..
6.
T-A- UZ%klu. Candidate or
Scalar PIs.tic Metal Properties Under Variation. of
St me tul.
7. PrOf.-Ior
@N.A-@ 1 On Some 44--till- of the Flow
.
Around porous W&LIg,
Card 2/5
5 S it 7
TITLE: n t 'rh e o rv ct h i-@ T nta6 p ae o f & 7: 1 a n ea ri:, _- n a rT
of Liquid Y zeorii nachal -nogo li@.hastka ploskov Ir-mi-nar-
noy stru.: zaidkosti)
PERIODICAL: Dopovidi Akade Mi4 nauk Ukrains,'Kci Rsrl, 1958r 1-Ir 7,
1 -
PP 702-7C6 (uSSR.)
ABSTRACT: Problems on the free and tuzbu!_-_nt Jets have been treated
by Schlicht-ing and Abramovich (Ref, 2) .71Th the
aid of the beundary laye-r equaUors, The solutions found,
howe-
ver, are Pot. adkiquate -for the Initial space of a jet.,
because they do not t@,ke into account sone factors, "There-
lore, th.@@ auttior @xpounds @he theory of the initial space of
a jet into a semispacr, occupied by the Fame liquid
using arproximate equations .--n the effects of acr-el-
eration -and viscosity component's are taken into consider-
ation. The ncticn Throualhout 'he entire domain is assumed
to be re8ular and plane )arallei. The authcr derives ap-
proximate equatlicn3 for a plane ii-,otion of a viszous ircom-
pres@ible liq,_,@_.d w@.ich a-Tc- reduced. for the pres.=-are, to
the Laplacp equation, and t1his is sGlved b,T Fourier's
me th od -Anal,-zin@- t*,ie sulution, the author states that
the pressure proves 4-C. b_@ VaT4abie, and a usually in-ade as-
Card 1/3 sumption as 'rhe zonstancv of p-ressure is applicable
N-58-7-4/27
On the Theory of the initial Space of a Plane Lar.-Arar Jet of Liquid
only for cases when the pressure in the cross section of
the inflow aperture is equal to that of the medium at in-
finity. For this particiilar case, the author derives a
simplified expression for the length of the jet -.ore of
almost constant velocities. The author solves the equa-
tion for the principal velocity component, a non-honogen-
eous equation of the one-dimensional theory of heat con-
ductivity., using the methods of operational calculus.
There are 5 "-*;.viet references.
A9SOCIATION: Moskovskiy gosudarstvenny., universitet imeni 1'.V- Lomono-
sova (1'@,oscow State "Iniversity imeni ".V. Lomonosov)
Card 2/3
21-58-7-4/27
On the Theor,, of the Initial Space of a Plane Taminar Jet of Liquid
PRESENTZOD: By Member of the AS UkrSSR, A.Yu. Ishlinskiy
SUM*ITTED: January 2-2, 1958
NOTE: Russian title and Russian names of individuals and insti-
tutions appearing in this article have been used in the
transliteration
1. Liquid jets-.--Theoz-y 2. Fourier's Series--Applications
Card 3/3
SOV/179-59--2-1/40
AUTHOR'- Slezkin.
TITIE: On the Theory of Gas Flow in a Layer Between the Front of
the Shook Wave and the Blunt Edge of a Rotating Body
(K teorii techeniya gaza v sloye mezhdu poverkhnostlyu
udarnoy voIny i prituplennoy poverkhnostlyu tela vrashcheniya)
PERIODICAL: Izvestiya Akademii nauk SSSR OTN, Mekhanika i mashino-
stroyeniye, 1959, Nr 2, PP 3-12 (USSR)
ABSTRACT: A method of investigation of the shock wave is described
in the article. The layer of gas is divided into the sep-
arate sections which are investigated consecutively, to
which the linear equations are applied. The velocity of the
gas U. is considered as being directed along the axis of
symmetry of the body, which is assumed to be stationary (fig-
ure on P 7). The formulae (1.1) are defined for an instant
when the shock wave iB affect1ug a layer (denoted by index A),
the thickness of which is h . The maximum value of the'
modulus U., is defined by Eq (1.2). The relationship of
viscosity and density 1L@p in the layer is not the same as
as T a 9 00 due. to the increase of the
> TC0 FA> 9
coefficient of viscosity together with an increase of temper-
Card 1/4 ature, i.e. -pA> ji0o . Therefore, It can be taken that
8(-)V./1?9- 59-2-3 /40
On the Theory of Gas Flow in a Layer Between the Front of the Shock
Wave and the B--lmt Edge of a Rotating'Body
number obtained from Eq (2.2) will describe the motion of
as in the layer, the parameters of which are shown in Eqs
2.6). In order to transform the formula (2,2) into the
@
linear equations9 the variables (3.1) are substituted into
Eq (2.2). Thus the formula (3.?) can be derived which can
also be written as Eq (3.8), when P, = 1 +-ep Nq 3.5).
The dynamic conditions of the front of the wave, in general
are defined as Eq (4.1),)which in the case of a plane wave,
can be shown as Eqs (4. 1, (4.3) and (4.4). The projection
of the vector of the tension on the normal Tnn and the
tangent T ns is given in Eq (4.5) which becomes Eq (4.6)
for the parameters (2.1). The expression (3.6) for the par-
ticular case when the density varies, (Zan be written as
Eq (5-1) for the conditions (5.2). Its solution can be shown
as Eqs (5-3) to (5.6) with the characteristic values U,, and
TB shown in Eqs (5.9). while the approximate value of den-
sity can be calculated from Eq (5.10). When the distance is
taken as that of the livider part of the layer., the velocity
Card 3/4
3011/1'@9-59-2-1/40
On the Theory of Gas Flow in a Layer Between the Front of the Shock
Wave and the B-l'unt -)f a Rotating Body
U increases together with an increase of the Reynolds num-
bgr (Eq 5.11), while the latter decreases near tho axis of
symmetry. Thus the above equations define more accurately
the conditions at the point near the axis. These conditions
can be found from the above equations when x = 0 c4
0 - 1/2 V and 0 = 1/2 ?1 are substituted in EqS (6.1) and
(6.4). Then E (5.6) can be written as Eq (6.5) and the
final formula N16) can be derived, which describes the
required conditions. There is 1 figure. and 8 Soviet refer-
ences.
SUBMITTED: February 17, 1.958.
Card 4/4
SISZKIN. N.A.
Applying Oseen's method to plane problem in the flow of a heated
gas. Vest Moak. un. Ser. mat., mekh., astron. fiz., khim. 14 no.2:
39-42 159 1. O(IU 13:3)
1. Kafedra aeromakhaniki i gazovoy dinamiki Moskovskogo gosuniver-
siteta.
(Gas flow)
L 16728-63 EPR/EPA(b)/EPF(e)/&IT(I)/U~(-n)-2/13DS --AFnCASDAJ-P(cY1!8V---
FS-4/7cl-4/Pr-4/@?u-4 WW
S/14/63/000/004/015/064,
AUTHOR: Slezkin N. A.
TITLE 0*0Tn"u"s"e"o?@TTnearized equations fqr studying m tion of gas., with
T
allowance for viscosity and heat'conductivity
PERIODICAL: Referativnyy zhurnal, Mekhanika., no. 4,, 1963, 71,,abstract 4B488
(Bull,math. Soo. sci. math* et phys, RPR .4, no. 1960,@ 85--92)
TEKT: Concepts on the possibility.and expediency ofusing linearized equations,
particularly the Reynolds-and Ozeyen type ones, for studying currents in the layer .
of a viscous and heat-conducting gas are presented. A condlu6ion is given foi four
different systems of such equations and a brief survey is made of reports by the
author in vhich the pertinent equations were used for-solving actual problems. So
M. Targ.
[Abstracter's note: Complete translation.]
Card 1/1
INE1,1ASOV, Aleksraidr Ivanovicb [deceased); PAVLIKHINA, M.A.; SEKERM6
ZU-11KOVICH, Ya..I., otv. red. toma; KWILISHCHIKOVA,, Ye.A.,,
red.i red.; RAIRTOV, L.P., red.; RYVK311, A.Z..,
red. izd-va; ASTAFfYEVA, G.A., tekhn. red.
(Collected works] Sobranie sochinenii. Moskva, Izd-vo Akad.
nauk SSSR. Vol.l. 1961. 442 p. (MIRA 15:1)
(Aerodynamics) (Hydrodynamics)
NEKI@ASOV, Alel,,sandr I-vanovich, adev ik; PAVLIKIIDIA, M.A.
TUPOIEVY A.11., akadeir-ik, otv. red. tona; ;'-7lJl,'IL'3FCHIIYOVA,
Ye.A., red.; S&dRZE-Zh'l*'KUVICH, Ya.I., -z-ed.:-SLHZKIN, R.A,
red.; SJ11d,1011, L.P., red.; GORSHKOV., G.B., red,izd-va;
NOVICHKOVAI, N.D., tekhn. red.
(Collected works]Sobranie sochinenii. Moskva., lzd-vc A]-,ad,
nauh S'SSR. Vol.2. 1962. 706 p. (MIRA 15:12)
(FITYsics) (Mechanics) (Ilatheraticv)
- SLEZKININ.A.1 doktor fiz.-matem.nauk,prof.; KORZHAYEV, S.A.
- -
Method for designing kydraulic and T)newz-,atic conveying units
suggested by.A.E. SmDldyroy. JzY. ARSSM 'Otd.tekh.nauk V16kh.
I wshinostr'.- =4-1:1-98-2W Ja-F 162. NM 150)
1. Foskovskiy Fosudarstvennyy universitet.
(Hydraulic conveying)(Pneumatic-tube transportation)
- - SLEZKINP N.A.
Kinematic and dynamic characteristics of a polyatomic molecule.
Vest.Mosk.un.Ser. 1: Mat., mekh. 18 no-3:72-81 My-Te 163.
(MIRA 16:6)
J. Wedra gidrodinamiki Moskovskogo universiteta.
(Molecular dynamics)
SLE27KIN. N.A.
Rernarks on 7.:@. -`@trashininals articles. izv. AN SSSR. 14ekh. no.l:
203-205 Ja-F 165. (MIRA 18:5)
SLKZKIN, V.A.
Experience in the use of values in gas pipelines. Gaz.
prom. 4 no-3:50-51 Mr '59. (MIRA 12:5)
(Gas. Natural--Pipelines) (valves)
SLEZXMIA, A.
------Pron the whole heart. Prom.koop. 13 no-1:35 Ja 159.
(MIRA 12'2)
1. Chlen arteli invalidov "Neva," Leningrpd.
(Vocational rehabilitation)
-r M, T-- -- -
Agriculture & Plant & Animal industry.
Hog farm of the "Smychka" State Farm. Saratovskoe obl. gos. izd-vo, 1951.
9. Monthl List of Russian Accessions, Library of Congress, April -1959, Uncl.
2
KLYUCHIKOV) V.N.; SLEMINA, L.I.; KOPSHITSER, I.Z.; SHUSTIKOVA, A.G.
Clinicall and genea-logica- studies of the family of a patient
with Thomsen's myotonia. Zhur. nevr. i psikh. 63 no.9:1313-
1319 163. (MIRA 17:8)
1. Klinika nervnykh bolezney Yaroslavskogo meditsinsicogo in-
stituta (zav. kafedroy - dotsent V.N. Klychikov) i nervnoye
otdeleniye (zav. A.G. Shustikova) gorods'r-,Oy b)llnitsy No. 68
(glavnyy v-ach V.M. Knyazev), 11foskva.
LOBATSEVICH, N.; SLEZKINA, N.
Straight amplification receiver, V pom. radioliub. no.12.-15-20
162. (MIRA 16:10)
SLEZKOVA,-,V._A. Cand Med Sci -- (diss) "On the ptoblem of clinical pathaphysiologic&2
peculiarities during the course of severe forms of epilepsy.CAccording to
observations in childrents clinic)." Mos, 1957. 14 pp (Inst of Psychiatry, Min
of Health USSR), 200 copies M, 44-57, 101)
-38-
V.A.
of so-called "suliclinical -setsures" in !severe typen
1. ith sumary in Yreachl. 1 'pallch. 57 n-.?:
of a?
,,,,,P,, r.
876-910 157. Ic.9)
1. Inatitut pal,khtstrit Minti7-ferstve 7.4ravookhronentya !SS:,R (11!-, -
Prof. D-T).?edotor), Monkys
(VIL&PSY. case reportn.
subalin. seizures in se7eze caces (RU-31)
SLEZKOVA., V, A,, YAROVICH, F.P., KOLB111A. M.S.
School onnatorium for ner7o-Qs children In Frunze District.
Zhur. nevr. I T)sikh. 58 no.7:396 '58 (MIRA 11:7)
(YRUkZR DISTRICT-RANDICAPPED CHILDIM)
SIMEVA, N.D-... kand.med.nauk
Pneumoperitoneum and endoscopic methods of examination in
gynecology. Med.sestra 22 no.3:35-39 Mr163. (MIRA 16:6)
1. 1@ Instituta akusherstva i ginekologii Ministerstva zdra-
voolchraneniya RSFSR.9 Moskva.
(PNMfOPERITONEUM, ARTIFICIAL) (EUDOSCOPY)
(C.TMOLOGY)
ONUYRIYEV. I.A., Inzhener, otvetstvennyy redaktor; BAUMAN. V.A.. kandidat
tekhnichaskikh nauk. redaktor; DOKBROVSKIY, N.G., doktor tekhnicbs-
skikh nauk, professor, redaktor; IVANOV, V.A., inzhener, redaktor;
KOKISSAROV, A.Y., inzbener. redektor; KONCROV, A.V., professor,
redaktor; TROITSKIY. 1rh.L., kandidat tekhnicheskikb nauk. redaktor;
SIXZNIKOV. G.1, inzhener. redektor; PULIKINA. Ye.A.. tekhnicheskiy
T-Mffo'@, D V.S., tekhaicheskiy redaktor
[Handbook of construction mechanics] Spravochnik makhanike no
stroitalgetva. Koskvs, Gos. izd-vo lit-ry po stroit. I arkhttekturs,
1951. 1064 p. [Microfilm] (KLRA 10:2)
1. Russia (1923- U.S.S.R.) Gosudaretvennyy konitst po delam
stroitellatva.
(Building machinery)
V.
41*tor 3-ELYAW.
I-A, nnul,; 3 -;I@,: t t f-khti -
r@-,eskikh nn'Uk; P-Ye, tei@hn icesklm-r., aauk.,
j,-;,e kr vanl@ V,,, IR, -S .
i,loviwl. L-and-iivt
,,,Ps;kikh mt-,3r- G
doktnr tekhnicl -. ,ONlU.::RG, YuY., in7@erpr-,
,;jtCi)?,T'iK!Y, I.Ye, -orofens--". '.-ktcr tekbntohe,;*,,-kh nouk: GORDPI,
I.C.. @)rofeoqor; i)lr*;NTBSRG, Y."T., kaz4ldat tekt,7,ii-heeltrize-b nauk.,
j,,, -:iiTOV, V - V - , i n7hi-- Oe r, M G7. A . G. nd i a t te,@ r ski Ich
mqnk: Kll@ksoSiffill. D:-ofessr,,:-;
i. '
..heskikch nauk; kane-, t tekhnienac-t-- -@a 1, 17
tekhnie@hpnlrl'h nauk-, KU;;HU,",- 'a karld, i -
4@t telrl-ml -her- nat;k; LO--Oziuli. Ye.Vf., 11-1zhener-. I.V.,
i n7.q-!e.-.er; K-,@ I. Lltl. li. Im nd idis t te i Ich nauk ; 14A RTY Oll D.
ka llll@@-@qG. lf.Yn, kandidat tev*@ni--
14-!K@::oz;v, G-i.. Lr:lesn!yr, d-'-'--- teAhnir-berkile@i nank;
F.7.TRUS:-,'VfCF.
;otEont,-
doktor v@':@ hn,-cheskilrh rg,,- ,
'@@Pndidat telehai,@'t n fln!7,0!-
at'l-, DAN, or
- SAT:;@ ,
t-I!,hnlibeskikh nn0z, I . E.A., arclre4-!-@r, iiokl-or
"I.Y. STLOBODKIN, M-6- , inzInere-s SPrISYN. N.A
.,aUl.; I... M
J J:h
nrcf-onvor, dol-l"or te _1,,' T G ke t
r
ts*r.@,nl--:!he:3ktkb nauk, Til!M@, B.A., kandiat
TBTELOBJAW-1, I.M., kandidet t ell-hniche ski 10h MANSKIY.
@ I -,)r, `-kqF@Cr,
-inkt@nr 1-@llrr i neuk; Fv,(l)'--S V. T.
d::'@tor tekhnich9sl-!Trl,. -n-It-, kGonfirn;ed or npx@ card)