DEFINITION OF LOWER CRITICAL LOADS DURING LOCAL LOSS OF STABILITY OF THIN SHELLS

Formulas are derived, which determine lower critical loads for: (a) cylindrical shell under action of axial compression; (b) conical shell, compressed by force along the generatrices; (c) spherical shell and spheroid under action of uniform external pressure; and (d) oblate ellipsoid under internal...

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Bibliographic Details
Main Author: Sachenkov,A V
Format: Report
Language:English
Subjects:
ANISOTROPY
CONICAL BODIES
ELASTIC PROPERTIES
ELLIPSOIDS
EQUATIONS
LOADS(FORCES)
SHELLS(STRUCTURAL FORMS)
SPHERES
STABILITY
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Summary:Formulas are derived, which determine lower critical loads for: (a) cylindrical shell under action of axial compression; (b) conical shell, compressed by force along the generatrices; (c) spherical shell and spheroid under action of uniform external pressure; and (d) oblate ellipsoid under internal pressure. Edited machine trans. of Izvestiya Vysshikh Uchebnykh Zavedenii. Aviatsionnaya Tekhnika (USSR) 1962, v. 5, no. 4, p. 111-122.