NASA NTRS · 19660021325
Flexible case analysis for compressible solid propellant grain motors Status report
Abstract
Stiffness version of finite element method used for numerical analysis of small elementary regions of solid propellant grains
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Key, S. W.. 1966-04-01. Flexible case analysis for compressible solid propellant grain motors Status report. https://ntrs.nasa.gov/citations/19660021325
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