The effect of edge constraint on the buckling of sandwich and ring-stiffened 120 degree conical shells subjected to external pressure / by Gerald A. Cohen.

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Main Author: Cohen, Gerald A.
Corporate Authors: Aeronutronic Ford Corporation, Langley Research Center, United States. National Aeronautics and Space Administration
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, 1967.
Series:NASA contractor report ; NASA CR-795.
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Norlin Library - Government Information - US

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Call Number: NAS 1.26:795
NAS 1.26:795 Available Place a Hold