NASA NTRS · 19730046627
Nonlinear analysis of a shock-loaded membrane.
Abstract
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.
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Madden, R., Remington, P. J.. 1973-05-01. Nonlinear analysis of a shock-loaded membrane.. https://ntrs.nasa.gov/citations/19730046627
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