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Structural analysis of viscoelastic materials under thermal and pressure loadingTechnique computes stresses resulting from axisymmetric transient thermal loading in circular solid-propellant grain section with circular ports. Propellant is assumed to be linear, thermal rheologically simple, viscoelastic material; material properties are represented by exponential series in time.
Document ID
19730000301
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Chen, J. C.
Date Acquired
August 7, 2013
Publication Date
July 1, 1973
Subject Category
Mathematics And Information Sciences
Report/Patent Number
NPO-11727
Report Number: NPO-11727
Accession Number
73B10301
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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