Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure

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Report Number: ASD TDR 62-801
Author(s): Roberts, W. H., Finwall, P. E., White, R. W., Eldred, K. E.
Corporate Author(s): Northup Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-08
Pages: 337
Contract: AF 33(616)-8219
DoD Project: 1370
DoD Task: 137009
Identifier: AD0600234

Abstract:
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Provenance: Jim Kinney

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