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On the pressure requirements for structural response equationsFluctuating pressure requirements for calculation of flight vehicle vibration environments - structural response equations
Document ID
19650014529
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Rechtien, R. D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Structural Mechanics
Accession Number
65N24130
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STRUCTURAL DYNAMICS
FLIGHT VEHICLE
VIBRATIONAL STRESS
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