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Structural Analysis Model Validation Using Modal Test DataThe design of a structure which can survive a prescribed dynamic environment is generally based on the use of an analytical model of the structure. The modal test is employed to verify the analytical model. This paper is concerned with the involved validation process, taking into account modal test results from realistic complex spacecraft structural systems as examples to demonstrate the proposed validation procedure. Attention is given to a load analysis model definition, a pretest analysis and test/analysis model, and the correlation parameters. Coordinate transformation is considered along with mode identification, frequency orthogonality, effective mass, mode shape, local kinetic energy, modal force, strain energy, and modal forces by acceleration measurements. Two examples are used to illustrate the procedure.
Document ID
19860042142
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
Authors
J C Chen
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
J A Garba
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Publication Information
Publication: Proceedings of the Joint ASCE/ASME Conference
Publisher: American Society of Mechanical Engineers
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: Joint ASCE/ASME Mechanics Conference
Location: Albuquerque, NM
Country: US
Start Date: June 24, 1985
End Date: June 26, 1985
Sponsors: American Society of Mechanical Engineers, American Society of Civil Engineers
Accession Number
86A26880
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Public Use Permitted.

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