NASA NTRS · 19710026795
Acoustic Analysis of Solid Rocket Motor Cavities by a Finite Element Method
Abstract
Adaptation of NASTRAN program to solve acoustic mode problems of solid rocket motor cavities by finite element method
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Herting, D. N., Joseph, J. A., Kuusinen, L. R., Macneal, R. H.. 1971-09-01. Acoustic Analysis of Solid Rocket Motor Cavities by a Finite Element Method. https://ntrs.nasa.gov/citations/19710026795
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