SCIENTIFIC ABSTRACT MUSTARI, H. M. - MUSIAL, L.

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• Collection: Scientific Abstracts
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• Document Creation Date: November 2, 2016
• Document Release Date: March 14, 2001
• Sequence Number: 7
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT


\X @'N
UNIN14 AL Wo mill Vkd=wo & 0. DOWWANdu d
dw skmW dW he deak 1 0 1 Is do beaWay
tone d1hin sheUs of certain tnie& Izvestiya Kazan.
Filial. Akad. Nauk SSSR. Ser. Fiz.-Mat. Tehn. Nauk 1,
9-24 (1948). (Russian)
The authors present the application of MuNtari's theory
for finding the stresses in the boundary zone of shells
[Akad. Nauk SSSR. Prild. Mat. Meh. 12,129-136 (1948);
there Rev. 9, 547]. This paper begins with a summary of
the general theory, introduces certain simplifications and
gives an estimate of errors due to these simplifications. The
theory is applied to the following shells: (a) shells of revolu-
tion with a spherical shelf as a special case; (b) an elliptic
owc The coustructioci of a ab function for boundary
iioaea of AdIs is abo premented. T. Lew.
Aq 935--'-045
Sol J-.';thSTiW-'4

-:-: .,-I -, I -I
; . . , I
- . @ I z .

MUSqTAR4-rff.-Fr.'
Determining the deformation of medium shell surfaces subjected to
arbitrary bending. Trudy KKHTI no-13-.132-137 148.
(I. MIRA 12: 12 )
l.Kazanakly khimiko-tokhnologichaskiy institut im. S.M. Korova.
kafedra teoreticheskoy makhaniki.
(Elastic plates and shells)

UM/axisearlm mar/Aprr 49
@bobwlos -
Wthenatios - Applied
07- Nuslitatlve I=vestiggLtion of Strain in Elastlo
Sbells for Smal' Deformations and Arbitrary
Dleplacemente."@ Hh. M. Mushtari ', Fh@rs-ot,-cji
Inst, Kezar- Affiliate.. Acad Sci USSR.. 14 PP
"Priklad Matemat I Mekh" Vol XIII, Nc@ 2
Classifies probl,?zs of linear and rmilnear
-& arv of shellf; ia which the number @@f ty-pt)e
the
Is reduced tc a minimmm. in additicm t-- cases
cansidere'd by We i -Zaag- Chien, in wh'.3h alfferen-
tiation with respect to Gaussian :cordizateti'd5ces
2 A qT2
LNO/Ugineering (Centd) Mar/Aprr 49
not change the order of -7alues characterizing
deformation,- classification alGe includee
boundary effects not subjecte6 to this canditicn.
Jb+Ablishe6 regian of applicability of the
linear thecry in general and solutions of
boundary effect @ypes in particular. !=Iudes
certain problemS --T strain in average-vidth
shells and several oases in the integration a
equatiams of nonlinear theory. Submitted
18 J@n 48.

"MA'b"Ics - Shells* 11"tic Doe 49
Nonlinear Mechanics
*X=Iinear Theory of Equilibrium of the Boundary
Zone of an Elastic Shell,w Kh. M. Hushtari, Kazan
Cbefticotech Inst imeni S. X. Kirov, 3 PY
*Dak Ak Nauk SSSR" Vol L M , No 4
Derives equation for nonlinear equilibrium of bound-
ary zone in elastic shell. Comparison of linear i@d
aMlinear theory as applied to theoretical example
at cylindrical shell of constant thickness, radius"S
andjength 2L, resting 'on its terminal croes sections
x1owl L 'and L acted upon by uniform internal pressure
UM/Physics - Shells, Elastic (Contd) Dec 49,
shan substantial errors are obtained when linear
theory is used to determine edge effect in thin elss-
t1a shell. Submitted by Acad A. I. Nekrasaw
30 Sep 49.
40 -1
15509

tc,
XUAR* EL x TIW 8AWY go
me MIA0110 bum aftedat d do -1 L JZVes-
tiya Kazan. Filial. Akad. Nauk SSSR. Ser. Fiz.-Mat.
Tehn. Nauk 2, 39--52 (1950). (Russian)
This paper is a continuation of the author's resimch on
the tboory of elastic equifibrium of dWb with ar%trary
to [Akad. Nauk SSSR. tarm. mat. Meh. 13,
121AM (1949); these Rev. it, 693. The author begins with
a brief summary of a previous (unavailable) paper [Trudy,
Kazan. Himiko-Telmolog. Inst, 13 (1948)], where a pre-
stressed shell is subject to two successive deformations. The
author derives the equations of compatibility and those of
equilibrium for shells as above. He modifies his general
theory for special types of shells subject to certain kinds of
deformations. He divides the shells into two types: (1)
shells of small curvature, and (2) shells whose dimensionless
curvature is of the order of one. The deformations are
classified as follows: (a) the momentless deformation, where
the bending deformation is small as compared with thel
deformation of the middle surface, (b) a mixed deformation,
where deformations due to bending and of the middle surface
are of the same order, (c) a bending deformation. The author
discusses separately the most important cases which are
combinations of the type of a shell and various kinds of
initial, primary, and secondary deformations, before and at
the loss of stability. He also presents simplified equations of
notral e4aMbrium, tbe, determination, of criticall loads,
AWWWOK in, Partiewdar *Ab of revolution. T. LOW.

aMA"sics - sumile saysillbriam NOVAar n
OXL&stlc Xquillbrium, of Thin Shells With Initial
Intorrections in the'rors of the Middle Surfac*,@
mi. M. Nuattari, Kazan', Phyx Tech Insty Mason
AMIlate, Aced Sci TSSR I
wFrMad Mteast i NOW Vol XV, No 6, py 743-750
Derives the fundamental dependences of the theory of
eqM11 in thin shell* vhose asdian surface pos"smw
Wtial bucklings (40s ) of the order of the thick-
ases of the *bell. Considers the stressed state in
allatuned (oblate) shell of rotation v%th positive
,-Gmsian curvature under the action of external.
low
I=/Physics - Elastic Equilibrium Nov/Doe 51
(Coutd)
prossure, in the case vbere, the shell possesses
lai#al Imperfection of form. Derives a formula
fairldetg the upper lisit of crit pressure. Sub-
wftted 8 Mar 51.

'AR19 1ho
Determi
na
tion
De fle
of
atigns of Prilcl.lkt.Nekh,
Panel- Sum mrted 12(6)
755460
ky.ZjALt. Lc Ncwwductil e ,,
Ribs and,
w ami External 1353 0
keronauticus Presmwe
.114rch 1954 R'h-U- M1211btari I,V, SZ1 ;ky U.S.S.R.
Strength" of 16-16@@@e the-,problem the equation of compatability of
Materials deformations,is integrated with the aid of Fourier's method'and
-Gal
the [e-mail] equilibrium by the Bubnov . erkin mathod. The
value of the upp
Oi'critical pressure thus obtaUhad tallies well.
with that obt y@&.AL X91tun through integrating both
'

equations' @vith tk@ aid-of Bubnov-Galerkin mothocl.
-The value
of
the Ime ri crit cal pressura dalculated in accordance with
'Apitunov's formulae, differed considerably due to,incorre.at
fuifil.
ment of - tha conditions of comoatability of deformit
ed, o
4so point ut(that the@upperpritical pressure@obtaihA'
%
.
by'the i@th6is-li6s above Jxwc:@@: CZ@Lt
it* real. value . Y;rhile -the,

;D nu-mber of "iei=i- in th
r sat(re"' - -below due to,,an.
=1CF04@V
p
,,
,
Semps'. (01b1*1

Akk (44*, fl-L oz@" 00. A-S

SRTRR I
i

124 - 5 7 -1- 865
Translation from: Referati,@nyy zhurnal, Mekhanika, 1957, Nr 1. p 115 (USSR)
AUTHOR: Mushtari, Kh. M.
TITLE: Approximate Determination of the Reduction Coefficient of the
Reinforcement of a Fixed Plane and Cylindrical Plate Under
Axial Compression (Priblizhennoye opredeleniye
reduktsionnogo koeffLtsiyenta obshitki podkreplennoy
ploskoy i tsilindricheskoy ptastinki pri osevom szhatii)
PERIODICAL: Izv. Kazansk. fil. AN SSSR, ser. fiz.-matem. i tekhn.
n., 1955, Nr 7, pp 23-35.
ABSTRACT: Examination of the supercriticial deformation of a plate fixed
to an orthogonal network of stiffening ribs and compressed
in a single direction. The stresses in the central portion of
the surface are determined for various degrees of loadings,
and the reduction coefficients are determined; all of these
reasonings are basled on the energy method. One of the
alternate solutions relates to the case when the points of the
edge of the panel are not displaced relative to the corres-
ponding points of the ribs; in a second alternate the points
Card 112 on the edge of the panel are assumed to slide freely along

124 - S7-1-865
Approximate determination of the Reduction Coefficient (cont. )
the ribs. The reduction coefficients found for either alternate are found
to be quite similar. Also investigated are large deflections of a circular
cylindrical panel, subjected to compression along a generatrix, following
a loss of stability. The magnitudes of the lower critical stresses are
found for panels having different values of the initial curvature.
Theoretical and experimental data pertaining to the reduction coefficients
are compared.
A. S. Vo I'm ir
1. Plates--Stresses--Mathematical analysis 2 Plates
--Deformation--Theory 3. Approximate computations--Applications 4 CylinJ@-i:!al
panels--Deflections--Mathew,aticaI analysis
Card 212

124-57-1-&A
Translation from: Referativnyy zhurnal, Mekhanika, 1957, Nr I, p I IS (USSR)
AUTHORS: Kornishin, M.S., Mushtari, Kh.M.
TITLE: Stability of an Infinitely Long Slanting Cylindrical Panel Under
the Action of a Normal Uniform Pressure (Ustoychivost'
beskcnechno dlinnoy pologoy tsilindricheskoy paneli pod
deystvLyem normal'nogr, ravnomernogo davleniya)
PERIODICAL- Izv.Kazansk. fil. AN SSSR, ser. fiz.-matem. 1 tekhn. n.
1955, Nr 7, pp 36-50
ABSTRACT: The paper offers a theory of large deflections of an infinitely
long, slanting, circular cylindrical panel subjected to the action
of a uniform normal pressure from the convex side. The edges
of the panel are considered attached; the cases of hinged and
fixed attachments of the edges are examined. Equations are
written linking the deflection of the panel and the stresses at
the center of the surface with the intensity of the load; these
relationships a:ppear te be exact within the limits of the assump-
tions made in the theory of slanting shells. An exact analysis
is carried out for the character of the deformation of the panel
Card 1/2 having differing degrees of curvature. The conditions for the

114-57-1-864
Stability of an Infinitely Long Slanting Cylindrical Panel (cont. )
formation of a toop-shaped "deflection-versus-icad'' curve are found, and
the upper and lower values of the loading intensity are indicated. The effect
of initial deviations from the circular shape upon the comportment of the
panel are evaluated. It is shown than an initial antisymmetrical deflection
can strongly influence both the upper and the lower critical loading.
Some relationships for the exact solution of the given problem were
earlier obtained by I. G. Bubnov [ Tr. po teor,.i plastin (Studies on the
Theory of Plates), 1953, pp 282-284)
A.S. Vol'mir
Cylindrical planels--Stability--Mathematical analysis 2 Cylindrical panels
--Theory
Card 2/2

, /7 6 a-,-, , A-h. /;"-/.
USSR/Physics Shells FD-1663
Card 1/1 Pub. 85-15/16
Author Mushtari Kh. M. (Kazan')
Title Theory of stability of a spherical shell under the action of an external
pressure (in connection with the article of V. I. Feodos'yev of the same
title, ibid., Vol. 18, I-To 1, 1954)
Periodical Prikl. mat. i Tel:h., Vol. 19, 2@1-2,r,4, Mar-Apr 1955
Abstract The author cives a new solution to the problem of the lower critical pres-
suref@r a spherical shell, using V. I. Fecdos'yev's approxiintation of the
form of buc1cling by way of the ordinary procedure of integration by the
Bubnov-Galerkin method; however, here he applies the principle of rossible
displacements. It turns out that the solving equation obtained in this way
coincidesvith the equation by the Bubnov-Galerkin method i-P t@-- 1--t side
of the equation integra*,2d ir multiplied by the variation of the approxi-
mating function. Three references; e.g. Kh. M. Mushtari and R. G. Surkin,
"Nonlinear theory of stability of elast ic equilibrium of thin spherical
shell under the action oC uniformly distributed normal cxternal pressure,"
P%7-1, Vol 14, No 6, l9r)o.
Institution : Physicotechnical institute, Kazan Affiliate of Academy of Sciences USSR
Submitted : Mar,, - 2', 1954,

SOV/1 24- 57-4-4603
Translation from: Referativnyy zhurnal. Mekhanika, 1957, Nr 4, p 105 (USSR)
AUTHOR: Mushtari, Kh. M.
TITLE: Some Mathematical Problems of the Nonlinear Theory of the Stability
of Shallow Shells (Nekotoryye maternaticheskiye problemy nelineynoy
teorii ustoychivosti pologikh obolochek)
PERIODICAL: Tr. 3-go Vses. matern. s"yezda. Vol 1. Moscow, AN SSSR. 1956,
pp 207-208
ABSTRACT: Bibliographic entry
Card 1/1

SOV/ I &I - 58-5-5700
Translation from: Referativnyy zhurnal, Mekhanika, 1958, Nr 5, p 1 10 (USSR)
AUTHORS: Mushtari, Kh. M_Kurnishin, M. S.
T IT LE: On the Convergence of the Galerkin Method When Determtning
the Upper and the Lower Critical Load Limits in a Particular
Nonlinear Problem (0 skhodiM05ti metoda Galerkina pri oprede-
lenii verkhney i nizhney kriticheskikh nagruzok %, odnoy nelineynoy
zadache)
PERIODICAL: Izv. Kazansk. fil. AN SSSR. Ser. fiz. -matem. i tekhn n.
1956, Nr 10, pp 27-30
ABSTRACT: A shallow cylindrical shell of infinite length subjected to an
external uniform pressure is examined. By applying the
Bubnov-Galerkin method the authors calculate the upper (Pu)
and the lower (P.) critical loads for the given problem. On the
basis of the calculations performed it is demonstrated that in
case of a pin- j oint- supported shell, for a wide range of shell-
parameter variations, the Pu and Pe values can be determined
with sufficient accuracy for all practical purposes by the second
approximation. In the case of a clamped shell the Pu value is
Card 112 determined with sufficient accuracy by the second approximation,

SOV./I ?4--58 - 5 -5700
On the Convergence of the Gaterkin Method (cont. )
while the P. value requires four approximations. In the two cases mentioned
above the Bubnov-Galerkin method approximates the Pe value on the lower side
of the true value.
1. 1. Voro,,ich
1. C.yllindrical shells--Mechanical properties
2. Cylindrical shells--Mathematical analysis
Card 2/2

-T
PHASE I BOOK EXPLOITATION 367
-Mushtarl, Xh. M., and Gall-or, K. Z.
Nel-ineynaya teoriya uprugikh obolochek (The Nonlinear Theory of Elastic Shells)
Kazan, Tatkh1goizdat, 1957. 430 p. 1,000 copies printed.
Sponsoring Agency: Alrademlys nauk SSR. Kazanskiy filial.
Reap. Edo.: Mushtari, Kh. M., Doctor of Physical and Mathematical Sciences,
and Surkin, R. G., Candidate of Technical Sciences; Ed.:
Vozdvizhenskaya, M. Kh.; Tech. Edo.: Nedellka, G. N. and Sallkhova, A. S..
PURPOSE The book to intended for scientific workers, graduate students and
engineers working on the design of thin-walled structures. It may
.be used as a textbook for students of advanced university courses
speci-slizing in the theory of elasticity.
COVERAGE: The book deals with the general theory of elastic shells with large
displacements and small deformations and with its applIcation in
the investigation or the stability and large deflections or the
Card 1/10

The Nonlinear Theory or (Cont.) ., 367
elements or thin-valled structures. There are 198 book referencesp 128 Of
which are Soviet,, 50 English, 20 German. The introduction mentions a
Soviet personalities in connection vith their publications in the theory of
elasticity. They Include: Vlasov, V. Z.; Goldenveyzer,,A.L.;IAr*PjA1-; Tqav,A.;
Novozhilov.. V. V.; Illyush1n, A. A.; Bubnow,, I. G.; and Papkavich, P. F.
The authors or this monograph thank their coworkers of the MechaniCs Section
of the Kazan' Branch of the Academy of Sciences, USSR for their help in the
accumulation or material and In the prepwation of the manuscript. They in-
clude: Kornishyn, M. S; Sachenkov, A. V.; Surkin, R. G., IsshbsVeva, F. S.,
Krivosheyev, N. I.; Ganiyev, N. S. It is mentioned that paragmphs 1, 14 -23, 2 5 -
35-62 were written by Ch. M. Mushtari, paragmW 2-13, 24, 63-65 by
K. Z. Gallmov and 27-34 by I. V. SvirsklY.
TA= OE
CONTEM:
Introduction 3
1. Basic concepts and notations 7
Ch. I. Theory or the Deformation of Ohellp
2. Certain data from differential gecimetry 10
Card 2/jo

The Nonlinear Theory of (Cont.)
3. Deformation of a surface
4. Deformation of a shell
367
18
25
Ch. II. Equilibrium Equation in the Theory of Thin Shells for Smal I
Deformations and Arbitrary Deflections
5. Equilibrium equations in the theory of elasticity in orthogonal
curvilinear co@ztinates 29
6. Internal forces and moments. Reduction of stresses and external
forces to the middle surface of a deformed shell 32
7. Equilibrium equation of the shell in orthogonal curvilinear
coordinates 37
8. Boundary conditions 39
Ch. III. Elasticity Equations. Variational Equations of the Nonlinear
T.heory of Shells
9. Relationship between internal forces, moments and deformations of
the middle surfaces 50
10. Principle of possible displacements. Strain energy of a shell.
Rit.z method 53
Card 3/10

The Nonlinear Theor7 of (Cant.)
36T
U. Equations of the Bubinov-Galerkin method 66
12. Intro&uction of symm?trical-emponents or internal forces and
mnents - Stress function T3
13. Principle of possible stress change in a shell TT
Ch. IV. Classification of Problems in the Theor7 of Shells and
Simplification of its Fundamental Equations
14. Small deflection. Linear theory of shells 90
15. Mediun deflection of a shell. Theory of flat shells 96
16. Large deflection of a shell 104
Ch. V. General Tbgor7 of the Stability of Thin Shells
17. Basic equations in the theory of stability of shells 109
18. On the stability of flat shells with amsill deflection 122
19. On the stability of long cylindrical shells of circular
cross section 126
Ch. VI. Nonlinear Theory of Flat Shells
20. Flat shells with initial deformations
133
Card 4/10

The Nonlinear Theory of (Cont.)
367
21. Principle of possible displacements and the energy criterion of
flat shells 142
PP. Equations of the Bubnow-Galerkin method for the variational
principle of Lagrange 147
23. Variational equation of the mixed-type method 150
24. Application of the formula of statically possible stress changes
to the theory of flat shells 158
25. Basic equations for flat shells of revolution and cylindrical
shells 172
26: Flat shell as a plate with initial curvature. Basic equations
in oblique coordinates 181
Ch. VII. Certain Problems in the Theory of Stability and the Large
Deformations of Rectangle Plates
27. Theorem of P. F. PapkavIch on the convexity of the stability
regions of, a she@l under ccmbined action of acme loads 187
Card 5/10

The Nonlinear Theory of (Cont.)
367
28. Stability of bng plate under combined action of a 100gitUdInal
compression and shear 190
29. Determination of the reduction coefficient of an infinite plate
reinforced by a grid of ribs under longitudinal compression load 193
30. Deterninalon of the reduction coefficient under combined action
of compression and shear loods appUed to the edges of a plate 204
31. Determination of large deflections of a plate with finite
dimensions 210
Ch. VIII. On Certain Methods of Solution of Problems in the Theory of
Deformation of Circul Plates 1
32. Basic equations In the theory of symmetrical deformation of
slightly curved circulw plates. Application of the method of
power series 220
33. Method of successive approximation and method of small pareneters 225
34. Asymptotial solution of the problem of the behavior of circular
plates@wder large loads applied at the edges 231
Ch. IX. On the Stability of the Moment-Free Equilibrium Conditions of
Cylindrical Shells of Medium Length
Card6AO

The Nonlinear Theori of (Cant.)
367
35. Certain equations in the theory of flat cylindrical shells 238
36. On the stability of cylindrical shell with circular cross section
under axial compression and normal pressure 243
37. On the stability of a cylindrical shell of an arbitrary cross
section under longituAinal compression. Shell with elliptical cross
section . Corrugated shell 249
38. On the stability of a shell of circular cross section subjected
to torsion and to combined action of other loads 256
Ch. X. On the Stability, and Large Deflections of Closed Cylindrical
Shells of a Circular Cross Section TAtAInitial "Imperfections"
39. Concept of upper and lower critical stresses 267
40. Lower critical stresses under longitudinal compression. Necessary
modifications of the Ritz-Timoshenko method 270
41. Determination of the reduction coefficient of the covering of a
reinforced shell under axial compression 277
42. Determination of the lower critical load Of a shell under allround
compression 285
Card 7/10

The Nonlinear Theory of (Cont.)
367
43.- Determination of the upper critical load of a cylindrical shell
with initial imperfections under axial compression and all-round
external pressure 290
44. On the stability under torsion of a cylindrical shell with
initial Imperfections 297
45. Nonlinear theory of the edge effect in a cylindrical shell.
Effect of the initial edge deformation on the stability of the shell
under axial compression 3o4
Ch. XI. On Large Deflections of Flat Cylindrical Pauels
46. On the stability and large deflections of a long cylindrical plate
under uniforiLly distributed transversal load 309
47. On the convergence of the Galerkin method in the solution of the
problem of section 46 316
48. Cylindrical panel supported by flexible ribs in the tangent p1we
under normal pressure 320
49. Effect of asymmetric Imperfections on the deformation of flat
panels under transversal load 326
50. Deflection of a flat cylindrical panel with free supported
edges under uniform transversal load 330
Card 8/10

The Nonlinear Theory of (Cout.)
367
51- Experimental investigation of the deflection of a panel under
transversal load 334
Ch. XII. On the Stability and Large Deflection of Circular
Conical Shells
52. On the stability of a conical shell of a circular cross section
under longitudInal compression 338
53. On the stability of a conical shell under combined action of a
longitudinal compression and external normal pressure 342
54. On the stability of a conical shell of a variable thickness
under uniform external pressure 347
55. On the stability of circular conical shells under torsion 351
56. Lower critical load of a conical shell. Local stability
of shells 356
Ch. KIII. On the Stability and Large Deflections of Shells of
Revolution
57. On the stability of an axisymmetrical equilibrium of a
moment free shell of revolution 361
Card 9/10

The Nonlinear Theory of (Cont.) 36T
58. On an axisymmetrical deformation of a flat shell of revolution
under large deflections 36T
59. Flat spherical membrane under internal pressure 376
60. On male-Ing more precise the general theory of buckling of shells 381
61. On the lower critical pressure of a total spherical shell 385
62. Certain ccmments an the methods of solution of a problem
analyzed in section 61. 393
Ch. XV. On One Method of the Solution of Boundaa7 Problems of
Nonlinear Equations in the Theory of Flat Shells
63. Large deflections of the rectangular cylindrical panel rigidly
fixed at all edges 397
64. Exact solution in series farm for the panel hinged at all edges 407
65. Free supported cylindrical panel under uniform tension-compression
load and external normal pressure 416
References 419
AVAILABLE: Library of Congress (QA935-M96)
LK/Sup
June 26,1958
Card 10/10

-/J
AUTHOR: 20-1-9/U
TITLE: On the Inverso.Boundary Value Problems of the Nonlinear Tnsory
of flat Shells (Ob obratn. kh krayevykh sadachakh nalinoynoy
toorii pologikh-oboloohe7
PERIODICAL: Doklady Akad. Sauk SM, 1957,Vol-116,Nr.1, PP-.35-37 (USSR)
ABSTRACT: Lot the medus aur-faae 3 0 of a flat thin shell of constant density
t be obtained before it is loaded by a normal shift *0.
The,sathox, farmul.&tes two problems:
1. For a glven 3 determine an 80 such that for a given pressure p,
gi.ven parlpheral farces and given boundary. conditions tke *hell
&SSMM*g AL given fOrM.
Z.. Detexmime the press- e and strain for given S, wG, v which
satisfy the. carresponding boundary conditions.
As an-axanpla a problem of the type 1 is considered in detail,
xhare under several simplify-img assumptions the solution is
ought in form of a series. The concrete resluts of the very
anded calculations are only sketched.
M
ASSOCIATION: K&MI Branch of the Acad, Se. USSR (Kazanakiy filial AN SSSR)
PRESMIMBY: L. I- Se&w, Academician, April 3, 1,957
SLMNITTED: Februaz7 18, 195T
AVAILABLE: Libtary of Congress

jOV/179-59-2-15/40
AUTHOR: Muslitari. Kh. M. (Kazan')
TITLE: Bend-ing Theory of Medium Thickness Plates (Teoriya izgiba
plit sredney tolshchiny)
PERIODICAL: Izvestiya kkademii nauk SSSR GTN Mekhanika i masfti-no-
stroyeniye, 1959, Nr 2, pp 10?-113 NSSR)
ABSTRACT: The classical th ory of thin plates may lead to errors of
the order of h2/a compared with unity, wiiere 211 is the
thickness and a is the width of the plate. In the present
paper, terms of this order are retained, and quantities of
order bL4/a4 and higher are ne.crie:@tedl. Equations are
derived for maximum deflection, bending and twisting moments,
and shear forces. Numerical --onsiderati-)a off a supported
plate subjected to a sinusoidal load and having a = 6h
shows that compared with the ar,,curate solut-Lon of Vlasov
(Ref 4) the deflection given by the present solution is 2%
Card 112

SOV/179-59-' --15/4-0
Bending Theory of Medium Thic.!cness Plates
in error, whereas ttie classical solution -is in error.
There is 1 table and there are '? references, of which 5
are Soviet and 2 English.
SUBMITTED: January 6, 1959.
Card 2/2

AUTHORS: Klishtarf arj@-l

TITLE:
Theory Cf sluping
PEBIODI@AL-. iz-vestiya A--,uder- z-ai
nauk, Ye-dhar,!Ka i
pp 6c,--6-7 i.USSR'
ABSTRACT: The paper
The marhemati.,,-@---
s tab! she@
and 1 a ri'a -!1' -,,-3 --'ri
no-mal suresz@ In.
numeri-@alll.; rie-7 @'Ol e 7,;- J
stated i r, s r, --s ) e J-
(3, 5)) :in i the s imp. i i J e - ? 1@a-
11 j - 4. J -1
"1 1" -!1 11 - . -
of a clamped isc-tropic. siiejl w, i
a r e e r i @i e i -
qxPressinns , ii--
!P L i 21
a, -- c o r d i n c h P r-,, (,v, e n

rdin6 t@, ne Kir.-h
and arco

c , a C r, m ) ar 1 s ci ri-
A nul
:"a tab-ul.ted r,rL Dage 111, C)Lt@ a ,
112
p a g, e 6 t h e @ i f f e e a in o -,.) n

Ttiacry S I
The-j
ASSC)@'TA21011- k'- 7

KMISHO, M.S. (Kazan); MUSHTARI, Mb.M. (Kazan')
Algorithm of a solution of nonlinear problems in the theory of
sloping shells. Prikl. mat. i makh. 23 no.1:159-163 Jw-F '59-
(Elastic plates and shells) (KrRA 12:2)
(Differential equations. Partial)

66409
AUTHORS- Mushtari, Kh. M., Teregulov, I. G. soT/20-12e-6-13/63
TITLE: On the Theory of Shells of Moderate Thickness
PERIODICALi Doklady Akademii nauk SSSR, 1959, Vol 128, Nr 6, PP 1144-1147
(USS10
ABSTRACTz The authors based their investigations on the principle of
virtual displacements to derive the equations for the equi-
librium of shells. These equations make it then possible to
introduce simplifications of a predetermined accuracy. Moreover,
the problem of boundary conditions in the theory of thick plates
and shells is solved here. The first equation written down re-
fers to the virtual displacements of a shell (which is assumed
to be a three-dimensional body), and the equilibrium equations
referred to the nondeforued state are derived next. The static
boundary conditions are then specified. Hooke's Law is written
down in a generalized form. The authors then investigate the
linear problem more thoroughly; the error permissible is of the
order of deformation together with an error of the order of
magnitude h 2/R2. Here, R denotes the smaller radius of curva-
Card 1/2 ture of the surface, h being a constant. The computation course
e

66409
On the Theory of Shells of Moderate Thickness SOV/20-128-6-13/63
is followed up step by step. The equations derived here were
applied to the solution of problems concerning the flexure of a
circular plate with a radius a, and a rigid central disk with
radius b under the action of a unilateral uniform pressure q in
the region b< r S. hl/h < E/E', then theory 2) is
inapplicable; since condition (9) is not fulfilled and the
influence of transverse shear on the magnitude of the deflection
licable-
is negligibly small and, in this case, theory 1) is a
n
(b) if s = r + 1, for example, hl/h -v"F, E/E, - E3 , then
theory 2) is applicable and the correction to the deflection is
of the same order as that determined by theory 1): (c) if
s > r + 1, theory 2) is applicable: (d) if s = r + 1/2,
h' V_e /h - E/E', the filler can be termed rigid, and theory 2) is
applicable.
There are 5 references: 4 Soviet and I English.
SUBMITTED: May 7, IL960
Card 4/4

MUSIITARI, Kh..I.T.)- STMIKII!, R.G..
ear
tilch.nfiuk- nc.14-23 -3j'
(.811 1L; p (I

6
BOMVSM P. v PHASE I 1300K EXPL40ITATION SO V16 206
Konfe-rentalya po teor1l plastin I obolocheic. Kazan'. 1960.
Tru-dy Konferentaii po teorit plastin I obolochek, 24-29 cktrabr7a
1960. (Transactiona of.the Conference.on the Theory ofTlates
and Shells Held In Kazan', 24 to 29 October 1960 Kaza@
[1zd-vo Kazanskogo goeudarstvannogo universitetai-1961. @@6 p.-
1000 copies printed. I .
Sponsoring Agency: Akademiya nauk SSSR. Kazanskly filial. Kazanskly
gosudarstvennyy univeraltetim. V. 1. Ullyanova-Lanina.
Editorial Board: Kh. M. Mushtari, Editor; F. S. leanbayeva, Secretary;
N. A. Alumyae, V. V. Bolotin, A. S. Vollmir, N.,S. Ganlyev,
A. L. Golldenveyze4 N. A. Killehavakiy, M. S. Kornishin, .
A. 1. Lux;lye, 0. M. Savin, A. V. Sachenkov, 1. V@ Sv-lmkiy,
R. G. Surk1h, and A. P. Filippov. Ed.: V. 1. Al*kBagih;
Tech. Zd@:- Yu. P. Semenov.
PURPOSE: .The collection of art1clos Is intanded'for @aientlsta'and
engineers iho are Interested In the analysis of strength and
stability or shells.
Card 1/14

Transactions of the Conference (Pont.) SOV/6206
COVERAGE: The book is a collection of articles delivered at the
Conference on Plates and Shells hold in Kazan' from 24 to 2j
October 1960. The articles deal with the mathematical th3ox7
of plates and shells and Ito application to the solution, in
both linear and nonlinear formulations, of problqms of bending,
static and dynamic stability, and vibration of ragular'.and
sandwich plates and shellb 6f Various shapes under varioug
loadings in the elastic and plastic regions. An4ys2v io made
of tho behavior of plates and shells In fluidaj and the effect
of croop of the material is considero4. A numbo@ of papers
discuss problems associated with the development of effective
mathematical methods for solving problems In the theory of shelli.
Some of the reports propose algorithms for-the solution of problems
with the aid of electronic computers. A total of one hundred,
reports and notes were presented and discussed during the con-
ference. The reports are arranged alphabetically (Russian) by
the author's no e.
Card 2/14

Transactions of the Conference (Cont.) SOV/6206
Grigorenko, Ya. M. On the NonBymmetrical State of
Strese of a Conical Shell of Linearly Variable
Thickness 142
Diugach, M. I. Uniquenesas Cond]'tiona of Displacements
In Multiply Connect-ed Regions and Shells With
Openings 149
Illgainov, M. A., and Kh. M. MuSjitarj. Some Problems
of Static and Dyna-mT-c-75-t-ability of Sandwich Plates 155
-1 1
Kan, S. N. 'Y"hermal 3trotsoes 'x. a ('1rcular Conical Shell 164
Killehavskiy, N. A. kppruxi=_@7e Methods for Investigat-
ing Equilibrium a-rd Vibration of Shellsas "Discrete
Continual" Sys-tans 170
Kc,valenko, A.. D. Solut-lon, in 3peCial Functions of
Unsymmetrical-Deformation Prob.ems of Shallow
SDharlcal and Conluii Shall.s 177
Card 7/14

2LI LitoD 24536
S/179/61/000/002/001/017
E08 l/E I/* i
AUTHORs Mushtari, Kh.M., (Kazan')
TITLE: The general theory of shallow sandwich-type shells
PERIODICALs Izvestiya Akademii nauk SSSR. Otdelsniye tekhnicheskikh
nauk, Mekhanika i mashincstroyeniye, 1961, No.2,
pp. 24-29
TEXT: In the work so far carried out on the theory of 3-ply
shallow sandwich-type shells, it has been assumed that the shell in
of symmetrical construction. This assumption limits the region of
applicability of the theory. If, for instance, the temperatures of
the bearing layers (the two outside layers) are different, or if the
permitted stresses in theme layers differ in compression and tension,,
it is reasonable to take the bearing layers as having different
thicknesses, and as being constructed of different materials. The
paper develops the general theory of shallow shells so as to allow
for temperature effects and for unsymmetrical construction. It is
assumed that the normal component of the displacement of the shell
(the displacement in the z direction) in independent of z, and
that the Kirchhof hypothesis is applicable to the bearing layers
Card 1/2

24536
S/179/61/000/002/001/017
E081/E141
The general theory of shallow sandwich-type shells
in view of their high mechanical strength. The filler (the midile
layer) is assumed weak in shear, and all the layers are assumed
thin. on the basis of these assumptions. equations are given for
membrane stresses and for bending and twisting moments. Taking into
account the equilibrium equations and the work of deformation of the
filler and the bearing layers, the equations governing the behaviour
of the shell are obtained, Particular cases of these equations are
considered as followss a shell with very thin bearing layers;
a shell with a very pliable filler; a cylindrical shell; and a
shell with isotropic layers. Ih the latter case, the system of
basic equations reduces to three equations relating to the
deflection, stress and shear functions.
There are 4 referenceal 3 Soviet and I English.
The English language reference readsi
Ref.1t E. Reissner. Small bending and stretching of sandwich-type
shells. NACA, Technical Notes, 1949, No. 1832.
ASSOCIATION: Kazanskiy filial Akademii n&uk SSSR
Card'2/2 (Kaz^nl Branch, Academy of Sciences, USSR)
SUBMITTED.k May 7, 196o

1 SUIW W&W

/000/000/015/008
/87
AA
id-
t-,7.,@.. "Ve-ior &-@Pl b6lodhOki -@-t u
yusnc
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". O'd IA on
Ap P;F VIA zror@
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i
sw
W, At"W ZQ-' W.",I T a. -y- -W
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37146
S/179/62/000/001/016/u27
E081/--'535
0 C
"his h t (&azan'
ri CLE': On(- refinettient of tile anoroximate theory of sandwich
n1ates with filler core
Tzvesti.ya. otdcleniye tekliniches-
J@ij,Zjl IlaUk. Mokhanika i mashinostroyenive, no. 1, 1962,
12 --j - 130
T'-"T 'file :3aner is a continuation of 7)reviotis w-ork
I z v. I,N oTN, Mekhanika
( @(, J*. - i mashinostroyenive, 1960,
.\0.6) In tile thoorv of thin sirlL..Ile izxyer plates, it is usiial
to assume that stresses normal to tile surface have a negligible
effect on tile stresses narallel to the surface. On the other
hand, it has been assumed in some previous works thitt in a light
filler stresses parallel to tile surface have negligible effect
un sag. "his assumption applies if the moduli of elasticitv
Of Lhe core are smal L in the directLon of tile plaile in comparison
with the modulus in the transverse direction. However, inter-
mediate cases can arise in which all stresses are of the same
order of magnitude. The paper gives it refinement of tile theory
Card 1/2

one refinement of the approximate S/179/62/000/001/016/027
RO 8 1 / E r, -, 5
wiiich includes thi s c;tse. The layers are assumed to he ortho-
tronic with compressible core; the displacements in the filler
core are expressed approximately as cubic equations in z ajI d
in terms of' the displacements at the middle plane, and the
di-spla.cements in the upper and lower layers are written in
accordance with the I@irchhoff hypothesis of deformation. Allowing
for ske@.%r svmtaetric and -symmetric bending, for tho equilibrium
equaLions and for the compatibility of displacements at the
upper and lower surfaces of the core, equations are obtained
for stresses, beriding and displacement in the bearing layers.
fhe compression of a souare plate with freeLy SUPPorted edges
bv a force uniformly apnlied to all edges is discussed, and it
is found that if stresses parallel to the surface are neglected,
it gives as an answer a substantially lower critical stress
corresponding to plate failure. For a material with Paisson's
raLio of O./f, the lowering amounts to 25,"7. There is I table.
-iU.3NIITTED: September 11, 1901
Card 2/2

MUSHURI, Kh.M. (Kazan')
Theory of sandwich shallow shells with filler layers of variable
thickness. Izv.AN [e-mail].*kh. i mashinostr. no.4:
71-76 Jl-Ag 162. (MIRA 15:8)
1. Kazanskiy filial AN SSSR.
(Elastic plates and shells)

MUSHTARI, Kh.M. (Kazan')
Area of the application of approximate theories of sandwich plates
with nonsymmetric structure and a filler. Izv.AN SSSR.Mekh. i
mashinostr. no.5:176-178 3-0 163. (KRA 16:12)

KGRMSH.U:, M.S.; @&SHTARI, Kh.M., prof., doktor fiz.-mat. nauk,
otv. rea.
[Nonlinear proolems .4n the t:.eory of @lates and s-allow
shells and methods for their solution] Nelineinye zadac:i
teorii FL-istin i poloFrikh obolochek i mptody ikh resNenii-a.
I I (INI"-,A i'-.o)
oskva, lzd-vc,) 19@4. 19 1 p. -
M

ACCESSION NR: AP4026953 S/02513/64/004/001/0045/OOU
AUTHORs Mushtaris Rh M. (Kazan)
TITLE: Theory of flexure of a rectangular plate of variable thickness
SOURCE: Inzhonerny*y zhurnal, v* 4, no, 1, 1964, 45-49
TOPIC TAGS: flexure theory, rectangular plate, variable thickness plate, square
plate, uniformly distributed transverse load, maximum stress intensity, maximal
deflection, freely supported boundary, Poisson coefficient
ABSTRACT: The author studies the effect of a uniformly distributed transverse
load p applied to a square plate of variable thickness 2h on flexure. He is
concerned with determining a law for varying the thickness to achieve minimum
volume for the plate, given a maximum value for the stress intensity or maximal
deflection. This law is approximated by
f3 Cos t Cos iq + a,, (cos 4 cos 3TI + cos 3E cos q) + 1j., coo 3-3
and is, in the ideal casej,
to Cos a Cos (2)
Card 1/2

AC03SION NR: Ap4o26953
The deflections are assumed small,, the deformations elastic, and the boundary of
the plate freely supported. The author is indebted to N. K. Galimov for program-
ing this problem. Orige art* hast 25 formulas,
:ASSOCIATICti., none
SUBM1TTED: 2ojun63 DATE AOQs l5Apr64 ENCL# 00
SUB CODE: AP NO ERF SOV 1 000 OTHIRt
CQrd 2/2

MIMITAR., Kh.M.
@ y --I' ,.e b,-ii-@ g . -- @, , A;- , . " , ,E4 '. s@ ': w: *,.,.
Am Inverse prcblem @- ---t t,
variable thIck-n@-ss. ::@Zt-Z-.L. . 4 nl.311r'3-5]@ '- tL.. @
7 -Lo"

L-00755-67

T 1%36-67 EIWP(d) /E WT (m)/EWP(j6/EVjP C
V)A. I-jp(k) _ jjp(D@ _,jAj/D,j
A @A12@032964 SOURCE CQDEs UR/W8/66/600/002/0035/0047@'
AU-Ln0i: Galimov, N. X.; Mushtari, Hh. M.
GRG: none
TLITIE: 71heory of three-layer plates and shells, U
SOnCE: 'Kazan. Universitet. Issledovaniya po teorii plastin i obolochek. no. 2,
964
TOPIC TAGS: metal stress, shell deformation, metal deformation
A3-STRACT: -1ho authors derive equations for equilibrium and the conditions for Joint
deformations of the slanting shell'of an asymetric structure, considering the
transversal def ormalt-ion @_f th`ofil@ler. The tangential and normal displacements of the
middle surface of the filler, a shear function, and the transversal deformation of the
are takon as variables. The filler displacements are approximated by a power
c-4pansion of the normal coordinate. The buckling is approximated by a linear function
and the tangential displacements by a quadratic one. The filler shears are assumed to
be constant along the thickness. Zie stresses are reduced to the middle filler
surface; the deformations are assumedto be small, and the budding finite. The problem
of stability of a cylindrical shell with orthotropic filler with reduction, and with a i
rigid isotropic f' or without F(iduction is solved. Orig. art. bass 42 equations.
':@ ---, SUi3x Diaz. --jur,63/ 0,UG RLF1 011

-MUSHTAY)ff Atf
,
Killing mehinery safety attachments. Stan. i instr. 24 no.5t3l Ky '33.
(KLRA 6:6)
(Milling mchinos)

KUSHTAYBV, A.F.
Protective devices used in vertical milling machines. Stan.1
instr. 27 uo.12:30-31 D '56. (KLRA 10:2)
(Killing machines)

BOIRWINO AJ., lush.; KOROZOT. Iel., Lath,; KWINOT, V.A., Inch,; LAPIDUS,
A.S., Insh,; BNOT, T.S.. lush.; KATJYWT. LJ., inzh.; 'Wa4m.-.-
A.S. -Insh.; FROKOPOTICH. A.Ye., red.; SHMSMMINA, Ya,A,, red,
ts-iffwas.; MAMMA. Te.T., takhn. red.
(Modernization of planers, slotters, and broaching machines; a
guide] Nodernizatofts, strogallmyld6 dolbeshakh I protlashmM
stankey; rukovodlashchis materialy. Pod red, A,2. Prokopovicha.
Moskva, Goa, nauchno-takhn. izd-vo mashinostroit. lit-ry, 1957.
178 P. (KOA 11:8)
1. Moscow. Akepertmentallnyy naxwhuo-iseledovatellskiy institut metal-
lorexhushchikh stamftv.
(Machine tools)

BOLTUKHIN. A.K.; STIRLIN, S.Z.; 6EC
9USHTA2,W iJKOROZOV. I.I.: KUDINOV, V.A.;
KOKAKHOV, G.A.; AZARXV`ICm;7T' W.-, EMPUS-.-A.S.; PROKOPOVICH, A-re.,
redaktor; RZHAVINSKIY. Y.T.. redaktor izdatelletys; TIKRANOV. A.Ya..
tekhnicheekly redaktor
[Modernization of knee and column type milling machines; instructions]
Kodernizataiia konsollno-frezernykh stankov; rukovodieshchis materialy.
Pod red. A.B.Proicopovichs. Koskva, Goa. nauchno-takhn.izd-vo mashino-
stroit.lit-ry. 1957. 194 P. (KLRA 10:8)
1. Moscow. Kkaperimentallnvy nauchno-issladovatellskiy institut
metallorezhushchikh stankov
(Milling machines)

KUSHTAYNV. A.F.
Iffect of clearances In the elements of drives on the
smoothness of table displacements. Stan.i inetr- 31
no.8:9-12 Ag 160. (KIRA 13:8)
(Killing machines-Electric driving)

MUSHTAYLV, A.F.
Modern plano-milling machines; survey of foreign literature.
Stan.i instr. 32 no.8323-30 Ag 161. (IMPLA 14:8,
(14il-ling machines)

MUSHTAYCV,, A.F.
Gape in feed-mehanism drives of heavy plano-milling machi as
Stan.i instr. 33 no.2:11-16 F 162-. (KrRA 15:1)
(Feed mechanism)
(Milling machines)

LOVI, A., podpolkownik; SHUL'G&. N., podpolkovnik; KASURMY, B., mayor;
#-K@- or.
Simplifying the rules of fire for adMtsent from 82 sm. mortars;
discussion of an article by Lt. Colonel A. Chervonyt, Docent wA
Candidate of Technical Sciences, in no. 4. Voen.vest. 36 no.7:
53-60 ji 156. (W& 9: 8)
(Mortars (ordnance))
(Cherwonyt. A.)

)(USHTUKOVA. 0. Ta. ;. IBCRSHGMffSKATA. S.I., red.; JAVONEVSXAYA, L.G., tekhn.
0
[In the struggle for aconomw In the use of mterlals] 7 bor"be za
ekonom1tu materialov. Daningrad] lerdzdat, 1954. 59 P. (Novator7
laningradskol pronVehlemosti, no,6) (MIR& 11:7)
(Shoe industr7)

I @ " @ @ " / , - , , ",
IOSEV, I.P., TUZHIIKIII, I.H.: KUSHUWT,@.R*I.,,
---
Self-foaming porous plastics made of polyesters and dilsocyanates.
Diul.takh.-ekon.inform. no.2-30-32 158. (KIRA 11:4)
(Plastics)

MUSIAL, Albin (Krakow, Wyezynskiago 7/6)
Case of penetration of the human eye by Therosycon tesselatum.
Klin. oczn& 24 no.2:147-148 1954.
(BYX. wounds and injuries.
*penetration by Theroviyeon tesselatum)
(LUGHESI
*Theromyson tessels.tum, penetration In human eye)

EMRM MEDICA See 12 Vol 13/8 Ophthalmology Aug 59
ravajoro - catania
1295. TI(E TIfERAPEuTIC RESI--!LTS OF NITRO('.RANUI-OGFN' TREAT&TENT,
ON TBE BASIS OF 2.5 YEAM' CLINICAL 1':XPVlilrN(-I-: IN OVER I-M
CASFS - Wyniki lerzenia iperytem azotIlWyn) na PUd5taW1f' 2.5-letnii-gi) jj().4-
wiadczenla klinicznego w ponad 150 prz.-,-padkach - M u s i a l' A. Oddz.
Ocznego P.S. K.. Krak6w - KLIN. OCZNA 1957, 2TrTTM"- 7T.F
On the basis of Aleksandrowiez's works concerning the anti -inflammatory vffevt of
nitrogranulogen in various morbid processes, such a treatment for eye diseases
was initiated in January, 1949. The (loses, 1/10 of those applied in America. were
administered according to the programme elaborated by Aleksandrowicz. In
September, 1949, at the Congress of the Polish Ophthalmological Society in Cracow.
the therapeutical results In over 40 cases were discussed. Up to the present inmovnt,
the number of patients treated with nit roll ranu logen exceeds 150. The results are
encouraging.

E
CERPTA MEbICA Sea gy 59
X 12 @1 13/4 Ophthalmolo Apr
626, A LARVA OF THE VITREOUS BODY, THE CAUSE OF SEVERE
ENDOPHTHALMITIS LARVOSA - Larwa szklistki przyczyn@ cieikiego
zapalenia �r6dgalkowego. (Endophthalmitis lar-vosa) - M u s i a i A. Odd.
Oczn. P.S.K., Krak6w - KLIN1.OCZNA 1958. 28/2 (715-M) Illus. I
During the section of the eyeball which took place after removal of the eye with
endophthalmitis, a larva was found of undetermined kind. The host was a peasant
girl of 15 yr. The disease lasted about 9 months. Szmyt - Warsaw

MIAL, Andrzej - -- -
Some notes on coal deposits in Korea with regard to the coal mine
deposits in Sinr-Chlang and An-Dju. Przegl geol 10 no.6.316-318
Je 162.
1. Zjednoczenie Przedsiebiorstw Geologicznych, Warszawa.

I-ILI S L".1, Ajitoni
a@)uara,us *,;4t!l sf-ff trarsvosa@.'- f1r7-, nF
j
mandible frjr th- trea-@Rer.+, r.-f pr(--e,- ia Czas.
stomat. 18 n(-.5;447-501 MY'F)@.
1. Z za-k@adu
Kalow'r-ach J@7-. dr. F.

m,TJSIAL, Edward, mgr.inz.
On the selection of the proper cross-section installation pipes.
Wiad elektrotechn 30 no.2:46-47 F '62.
r-
1. Politechnika, Gdansk-

MUSIAL, Edward, mgr inz.
- - 1-11--l- -------
"The electric wireman; collection of information in questions
and answers" by F. Rozmus, W. Stanislawski. Reviewed by
Edward Musial. Wiad elektrotechn 32 no. 1:29 Ja 164.

MW.LAI, J .
For an interdepartmental accounts settlement. p. 260.
(P'rZr,GId Ij SKORZANY. Vol. 11, no. 10, Oct. 1956, Lo(jz, Poli,nel)
SO: Monthly List of East European Accessions (UAL) LC. Vol. 6, No. 12, Der. 1Q57.
Uncl.

BETAK., M,J, inz.;_14USIAL, J.
Development of two-layer panels at the Prazske cihelny
National Enterprise. Stavivo 41 no.10:356-358 0 163.

MUSIAL, L.; CHOBOT, M.; PUDO, J.
Water pollution in the Rabe River. GoBp wodna 21 no.8:359 Ag 161.

MUSIAL, L.; FM, J.; LABUZ, W.
Water pollution of the Skawa River. Gosp wodna 21 no.8:360 Ag 161.

MUSIAL,
New derivatives of hydanton substituted in the rositiors 3,5. 1. p. 1115.
/IIC', API-1-
RC,CZ,PTIKI CMIII. (Pols a Akademia Nauk darszawal. Vol. 2, no. 5, 1959
p
Monthly List of East turope-an Accessions (EEAl LC, Vol. 8, no. 7, July 1959
Uncl.

- MUSIAL, Leopold
On new substituted hydantoin derivatives in the 3 and 5
positions. III. Rocz chemii 35 no.6:1651-1660 161.
1. Zaklad Chemii, Wyzsza Szkola Pedagogiczna, Krakow.

MUSLAL, Leopold; KGRGHODA , Maria jolante.
New hydantoin derivatives substututed in positions 3 and 5.
Pt. 4. Rocz chemii 36 no.11:1607-1614 162.
1. Katedra Chemii, Wyzsza Szkola Pedagogiczna, Fxakow.

MUSIAL, Leopold; STANIRC, Jadwiga
Now hydantoin substitution derivatives in positions 3 and 5.
Pt. 5. Rocz chemii. 37 no.6.6ZI,628 163.
1. Katedra Chemii, Wyzsza Szkola Pedagogiczna, Krakow,