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Nonlinear analysis of a shock-loaded membrane.Results from a computer method for analyzing the unsteady interaction of a fluid stream and a flat circular elastic membrane are presented. The loading on the membrane is assumed to be caused by the firing of a shock tube. The fluid pressures and velocities are determined from a scheme based on the numerical method of characteristics, and the membrane is analyzed using exact relations for membrane strain. The interactive solution is found to give peak stresses 40% lower than a solution which assumes a pressure invariant in space and time.
Document ID
19730046627
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Madden, R.
Remington, P. J.
(Bolt Beranek and Newman, Inc. Cambridge, Mass., United States)
Date Acquired
August 7, 2013
Publication Date
May 1, 1973
Subject Category
Structural Mechanics
Report/Patent Number
AIAA PAPER 73-443
Meeting Information
Meeting: Aerodynamic Deceleration Systems Conference
Location: Palm Springs, CA
Start Date: May 21, 1973
End Date: May 23, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
73A31429
Funding Number(s)
CONTRACT_GRANT: NAS1-10024
Distribution Limits
Public
Copyright
Other

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