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Buckling of thin-walled circular cylinders, NASA SPACE VEHICLE DESIGN CRITERIA (Structures)

NASA/SP-8007, Seide*, P. and Weingarten*, V. I. and Peterson**, J.P., Buckling of thin-walled circular cylinders, NASA SPACE VEHICLE DESIGN CRITERIA (Structures), NASA (Washington, DC, United States), *University of Southern California, **NASA Langley Research Center., September,1965, pp. 56, Format(s): PDF 4550k

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Predicting buckling of thin walled, uniform stiffened and unstiffened circular cylindrical shells under static loading.
Keywords:structural mechanics, buckling, circular shells, cylindrical shells, reinforced shells, static loads,thin walled shells, axial compression loads, bending, sandwich structures, torsion
CASI Document ID Number:69N23320
Subjects:Engineering: Structural Mechanics: Shells
ID Code:6
Deposited On:13 May 2002