SCIENTIFIC ABSTRACT MANEVICH, I.V. - MANEVICH, YE.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R001032120013-8
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: November 2, 2016
• Document Release Date: March 13, 2001
• Sequence Number: 13
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

ANFINDV, A.S., inzh.; HAMVICH I V , iazh.
Band cantilever dunper. Bezop.truda v prom- 3 no-10:33
0 159. (MIRA 13:2)
1. Treat Volchanslwgoll.
(Coal mining machinery)

ANDRIANOV, K.A.; MWVICH, I.Ya.
Synthesis and properties of acid salts of methylphospbinic acid.
Zhur.noorg.khim. 9 no.1t210-212 Ja 164. (KRA 17:2)
1. Institut alementoorganichookikh soyadinanij AN SSSR i Indtitat ob-
shchey i neorganicheskoy khimii imeni N.S.Kurnakova AN SSSR.

ANDRIANOV, K.A.;
Acid salts Of -neth.v%'--.'
no.3:596-600
1. tit-,@ t

IGH, 1.Z. (Ry&zan')
Behavior of integral curves of a system of homogeneous differential
equations with continuous right-hand parts* Izv. Vys, ucheb. sav.0,
mat. no,3sll7-120 165. (MIRA 18M

t
I "1 1. 11 @./;I-.II'- /- I
KWPOTOV. :jAMIA@ ; TSVMV. V.
Combined promius-flxad wage system, Sots. trud no.4:117-123 Ap '57.
(Wws)

PETROV, K.M.; DYAKONOV, V.I.; FADLYEV, I.G.; SEMENENKO, P.P.; KRYUKOV, L.G.;
Frinimali uchastiye: PASTUKHOV, A.I.; SHISHKINA, N.I.;
PAZDNIKOVA, T.S.; CHIRKOVA, S.H.; KARELISKAYA, T.A.,; LOPTEV, A.A.;
DZEMYAN,, S.K.; ISUPOV, V.F.; BELYAKOV, A.I.; GUDCV, V.I.;
SUKHMAN, L.Ya.; SLESAREV, S.G.; GOLOVANOV, M.M.; GLAGOLENXO, V.V.1
ISUPOVA,, T.A.; ZYABLITSEVA, M.A.; KAMENSKAYA, G.A.; POMUKHIN, M.G.;
UTKIM,, V.A.; MAIEVICH, L.Q.-
Vacuum treatment of alloyed open hearth steel. Stall 22 no.2:3-13-
317 F 162. (MIRA 15:2)
1. Urallakiy nauchno-iseledavatellskiy institut chernykh metauov
(for Fastukhov, Shishkina., Pazdaikova., Chirkoval Karellskayal,
Loptev,, Dzemyan). 2. Metallurgicheskiy kombinat im. A.K. Serova
(for Isupov, Belyakov, Gudov, Sukbman, Slesarev, Golovanov,
Glagolenko, Isupova, Zyablitseva, Kamenskaya). 3. 6-y Gosudar-
stvennyy podshipnikovyy zavod (for Pomukhin Utkina, Manevich).
(Steel--Metall-urgyi
(Vacuum metallurgy)

SEWLYAKOV, Yu.A.; MANSVICH, L.I.
-4` 1
Certain .'the stability of a flat bend. Dop. AN UM
no.6:627-630 '58. (MIRA 11:9)
l.Dnepropetrovski3r universitet. Predstavil akademik AN USSR G.N.
Savin [H.M. Sevin].
(Elastic rode and wires)

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rl@ V
27049
2-C01 S/021/60/000/005/005/015
1191
Li
D210/0304
AUTHORS: Shevlyakov, Yu.A., and Manevych, L.I.
TITLE: The stability of a cylindrica@ shel-l-u-nder bending
PERIODICAL: Akademiya nauk ukrayins*koyi RSR, Dopovidi, no. 5, 1960,
605-608
TEXT: The ;rticle deals with determining the lower critical (buckling)
stress of a thin-walled cylindrical shell under pure bending. The
problem is solved by approximation using the basic non-linear equations
of the theory of elasticity. The critical state is given by
so duo T., where v 0 = 0 for x = 0 and
ax = h x The x-axis lies along
20 - av, - Wo -,74. a generator, the y-axis along
9 TU Th the tangent to the excess load,
and the z-axis towards She Sen-
10 !lt-10 + IUQ - 0. ter of curvaturee 09 C I @'
XV 0'r Oy x y z
Card 1/6

27049
S/021/60/000/005/005/015
The stability of 0210/0304
are the deformations, of the central plane, u0, vot w0are the displace-
ments in the x,y,z directions respectively, H and e are rZapectively the
radius and length of the shell, %/'is Poisson's coefficien 6-0 = T0
is the normal stress. Also, X X
h
cr O= H = 67' con X (3) where M is the
x W o R
bending moment, W in the support moment Lyo M2h h is'the.thickness
11@ R
of the shell* Integration and substitution given for the displacements
U 00 X COSY Investigation of the stability
Y 2 gives (Eqs. 5 and 6 see next
card)
VO 00 z x) sin (4)
2EJ? R
W. [x (I x) NRIJ Cos
Card 2/6 , 2ER R

27049
S/021/60/OB6f##5fM5/0l5
The stability of a... D210/ ,0304 "k -
a2w 2 a2w a1w I a2w where Z is the
Eh OX ay ax. ae hi Txi (5) stress7function,
R for the central
Dv'v'w - a'(D. a1w - 2 a2(D a?w + fo a1w I a-'(D plane, and
GO ax-2 OT(@)y @7X -ay J.V2 &1Z (6) Eh2
X D= - 2
in the cylindrical rigidity. w and are written
W = w I + w 0 where w I and A are respectively the Aeflection
+ (7) with respect to thenormaL and the stress function
which characterizes the bulging of the shell,
.and 0 R2 Cos 'X . If E71.5R the boundary
0
conditions may be ignored. The first approximation for w I given in the
zone of compression 'XX
W, = f1i Cos Cos Y + a cos + b cos Cos (10)
Card 3/6 V X IR
X,

27049
8/021/60/000/005/005/015
The stability of a.-* D210/D304
and in the zone of tension w 0. x and A Y are longitudinal semi-waves
in the x and Y directions, ft al b, are dimensionless parameters. Solving
for I gives
co 1E + gcw(@ + 9. ca
@+F ,
44 + I.,., C,* 3A@ +
+
(.1; , + +
+ + +
+
T_
as + + (1@ - W,
4 I..M !?.
+
Card 4/6 (@'

27049
S/021/60/000/003/003/015
The stability of a... D210/0304
where the g, are found from the boundary conditions in the usual way.
The energy equation for a general system Is )a ) I + 32 - V' where
3 1 is the energy of deformation of the central plane, D2 'a the energy
of bending, and V in the potential of external forces. Ignoring smald
quantities [Abstractor's Note:
,.16 R 2 Y (a 4. b)2 + 4a'bs as Symbols not ex-
(I + 62)1 + + SF62-P + plainedD . The
energy criterion
b2 17 1 01 of equilibrium in
+ T9 -+6 1) 2 + -12-8 + T2 - 2-5 6(1 + 8a@'I+ j ()2)2 Eq. 13
(12) (see next card)
(a + b) + 8a), 2 +
- Ti -+-62) T2-8 3 0
T8 0 - [(I + 61)1 + 32 (Al + bl)] - 0,225. co, + W).
Card 5/6

27049
S/,921/60/000/005/005/015
The stability of a.*. D210/0304
a.9, aq, a,9' a3, aa, 0. (13) from wbich can be found
a; - aq ab' aa @-j the relationship between
the load parameter for
pure bending and the uniform axial compression in the post-critical
stage, Hence, the lower critical (buckling) stress stay be found. The
load parameter in this case in 0.26. and thus in obtained the approxima-
tion formula Eh with uniform axial compression
(ro = 0,26 R (15) 70 1= 0, is -a). (15A)
0 R
There are 2 Soviet-bloc referqncess
ASSOCIATION: Dnipropetrovalkyy derzhavnyy universytet (State Univer8ity
of Dnepropetrovsk)
PRESEITED: by Academician AS UkrSSR H.M. Savin
SUBMITTED: June 17, 1959
Card 6/6

(I U t Lj ic, k , /-. I
FAROVSM, P. V. PHASE I BOOK EXPL40ITATION BOV16 206
Konferentelya po teoril plastin i obolachek. Kazan'. 1960.
Trudy Konferentsil po teorli plastin I obolochek, 24-29 oktyabx7a
1960. (Transactions of.the Confer-ence.on the Theory of@Plates
and Shells Held in Kazan', 24 to 29 October 196o Kazan
[Izd-vo Kazanskogo gosudarstvennogo unlyarsitetal-1961. 4k p:
1000 copies printed.
Sponsoring Agency: Akademiya nauk SSSR. Kazanskiy filial. Kazanskly
gosudarstvennyy universitetlim. V. I. Ullyanova-Lonina.
Editorial Board: Kh. M. Mushtari, Editor; F. S. leanbayeva, Secretary;
N. A. Aiumyae, V. V. Bolotin, A. S. VollmiW, N.iS.-Ganiyev,
A. L. Golldenveyzer, N. A. Killchevskly, M. S. Kornishin, .
A. I Lw@lye, 0. N. Savin, A. V. Sachenkov,''I. V. Svirskiy,
R. 0: Suriciii, and A. P. Filippov. Ed.: V. 1. Alek3agjn;
Tech. Ed-:- Yu. P. Semenov.
PURPOSE: The collection of articles in Intended'for sdientista'and
engineers iho are interested in the analysis of strength and
stability of shells.
Card 1/14

Transactions of the Conference (qont.) SOV/6206
COVERAGE: The book is a collection of articles delivered at the
Conference on Plates and Shells held in Kazan, from 24 to 2j
October 1960. The articles deal with the mathematfcal thaox7
of plates and shells and Its application to the solution, in
both linoar and nonlinear formulations, of-probloms of banding,
static and dynamic stability, and viDration of r6gular'.and
sandwich plates and shellb bf V&rious shapes under varioul
loadings In-the elastic and plastic regions. An4ys2a*ia made
of the behavior of plates and challs in fluidsj and the offeav
of creep of the material is coasidereo. 9 in=boi- of papers
discuss-problems associated with the development of affective
mathematical-methods-for solving problems in the theory of-shelli.
Some of the reports propose algoritkus for-the solution of problems
with the aid of'electronie computers. A total of one hundred,
reports and notes were presented and discussed during the con-
ference. The reports are arranged alphabotla&lly (Russian) by
the author's name.
Card 2/14

Transactions of the Conference (Cont.) sov/62o6
Makarov, B. P. On the Nonlinear Flutter of a Plate 220
Clamped by Its Circumference
Manevich, L On the Stability of a Cylindrical
611 Under lJonunifoxm Axial Compression 226
Mitkevich, V. M. Symmetrical Deformation of a
Stiffened Conical Shell 233
Mlshenykov, G. V. On the Dynamic Stability of a
Shallow Cylindrical Shell 239
-My-arsepp, P. V. On a Method for Investigating the
Behavior of Shells After Plastic Buckling 246
Obolaehvili, Ye. I. Positive Curvature Membrane Shells
A-ted on by Discontinuous External Forces 250
Pav laynen, Y. Ya. Membrane State of Stress of
tCircularl Translational Shells 2rA
Card 9/14

AUTHOR:
TITLE:
V,
1101, 1@21'
L, 28713
S/021/61/000/DO8/008/011
D210/D303
Manevych, L, I.
On the local stability of shells under non-uniform
loads
PERIODICALz Akademiya nauk Ukrayinalkoyi RSR. Dopovidi, no. 8,
1961, 1018-1021
TEXT: 1) A thin cylindrical shell of medium length is considered,
being in conditions of eccentric compreseion prior to loss of
stability. According to the momentless theory, the normal stresses
in the section is
o' = To + Ti Cos B = GO( 1 + rcos 3)
(1)
To being the stress of uniform compression, a-, the maximum bending
Card 1/6

On the local stability ...
28713
S/021/61/000/008/008/oll
D210/D303
stress, 8 the angle counted from the plane of bending if 6---.-0,
r->O and if cr0--;;,O,r-:PoDand a---@,Ir @ nveltigate
1cos 3. 2) T i
the stress, a system of non-linear equations is used which relate
to each other the additional forces and displacements in buckling.
The boundary conditions are satisfied in the integral sense. The
additional radial buckling is imagined in the form
w f.h cos aC- cos VR13 + ot cos !W-F + b cos 2M)COS k 3 (2)
A e. A13 A F. N. 7
where,4F, A are half wavelengths in the direction8F
,,B. Using the
Ritz-Papkovich method, one must find the solutions for several
values of k (0,2,4,6,8,10). Z-Ab8tractorls.note: An example of
partial solution for the stress function with k=2 follows, con-
sisting of 32 terms.7 The coefficients gi at-e determined in the
Card 2/ 6

On the local stability ...
28713
S/021/61/000/008/008/011
D210/D303
usual way. The terms cos 23 correspond to the part
g3loo's so g32
of additional axial force which has a comparatively large period
of change. The presence of such terms, due to the non-linear
effect, determines the influence of inhomogeneity of the stressed
stat-e on lower critical force. To calculate the upper critical
stress one puts a=b=O and does not take into account the terms
due to non-linearityof initial equations. The dimensionless pa-
rameter of total energy, computed according to the well known
formulae, according to A,S. Volmir (Ref. 3: Gibkiye plastinki I
obolochki (Flexible Plates and Shells), Gostekhizdat, 1956, 52),
can be imagined in the form
0 '25r2 94 + r2 (1+922 _ 0,25a, (k,r) r 292 T X
(j+g2)212 48(1-v2
where
Card 3/6

On the local stability-.,_
9 I-A=3 - @ = Tr2Rh ;
At: /k2
13
28713
S102 61/000/008/008/011
D21 OYD303
r = f -cr JK= R
'f_h a,
The values of c( (k,(I are given in a table. The relation between
the critical st@esses of central and eccentric compression is
or = 1
_cLj Fk-,4-7 TO
(4)
When k increases, it is ct (k,,r)-->l for all values off', i.e. the
upper critical stress doea not depend on the eccentricity of
load. The same result car, be obtained by computing the energy
corresponding to the zone of maximum compression -Aj3/R