SCIENTIFIC ABSTRACT GRIGORYANTS, M.M. - GRIGORYEV, A.A.

• Document Type: CREST
• Collection: Scientific Abstracts
• Document Number (FOIA) /ESDN (CREST): CIA-RDP86-00513R000516810002-8
• Release Decision: RIF
• Original Classification: S
• Document Page Count: 100
• Document Creation Date: January 3, 2017
• Document Release Date: July 27, 2000
• Sequence Number: 2
• Publication Date: December 31, 1967
• Content Type: SCIENTIFIC ABSTRACT

GRIGOR'YANT5,,M.N.j podpolkoynik me~. aluxhby.
Onses of anioterto leptoopirosis in Tajikistan. Voen.-med.shur. noollt
80 N 156 , (MIRA 12: 1)
iTAMISTAN-LOTWPIROGIS)

11 CIL r I C'!

GRIGORIYANTS, N.M. (Karlkov)
Free oscillations of thin plates with calculation of the
inertia of rotatima Stroi. mekh. i rasch. soor. 3 no.
3:36-37 161. (KIRA 1416)
(Elastic plates and shells)
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23300-66 EWT(d)/EWT(M)/EWP(N)/EWP(V)/-,-WP(k)/EWA(h)/ETC(m','-,6 ljf(c'
AUTHORs Grigorlyants, N. M. (M=Ikov)
ITO/Em
ORG: Khar1kov Engineering-Construotion Institute (Kharlkovokiy inzhenerno-
stroitellnyy institut)
TITM: Equilibrium stability of' acylindrical shell utlom suddenly applied loadl/4
SOURCE* Prikladnaya mekhanikat v. 2, no. 29 19661 9-56
TOPTC TAGS% shell buckling, shell deformation, cylindrical shell structure, shell
lotru.ture stability
ABSTRAM: The axisymmetrio mode of buckling of a smooth cylindrical shell under a
suddenly applied axial load Is conaidered. Both tho radial inortial forces and Me
inertial forces inside the shell surface are included. By using the Galerkin method
for a freely supported shell, a system of two nonlinear differential equations is
obtained. These are solved approximately with the help of the methods described by
V. V. Bolotin (Dinar"oheakaya. ustoychivost' uprugikh sisteM9 GITTLt M.g 1956)t am
equations for the critical loade and corresponding deformation amplitudes are derived.
Orig. art* hast 2 figures and 36 formulas.
SUB COM 209 13/ MM DAM 21Apr65/ ORIG RM 003
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