Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure
Report Number: ASD TDR 62-801
Author: Roberts, W. H.
Author: Finwall, P. E.
Author: White, R. W.
Author: Eldred, K. E.
Corporate Author: Northup Corporation
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-08
Pages: 337
Contract: AF 33(616)-8219
Project: 1370
Task: 137009
AD Number: AD0600234
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Jim Kinney
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