Investigation of a Method for the Prediction of Vibratory Response and Stress in Typical Flight Vehicle Structure: Supplement I - Dynamic Modeling of Complex Structures

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Report Number: ASD TDR 62-801 Supplement I
Author(s): Roberts, W. H. , Finwall, P. E.
Laboratory: AF Flight Dynamics Laboratory
Corporate Report Number: NOR 63-139
Date of Publication: 1964-04
Pages: 249
Contract: AF 33(657)-10075
DoD Project: 1370
DoD Task: 137005
Identifier: AD0600234

Abstract:
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Provenance: Bombardier/Aero

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