NASA NTRS · 19730000301
Structural analysis of viscoelastic materials under thermal and pressure loading
Abstract
Technique 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.
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Chen, J. C.. 1973-07-01. Structural analysis of viscoelastic materials under thermal and pressure loading. https://ntrs.nasa.gov/citations/19730000301
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