Nonlinear thermoviscoelastic analysis of solid propellant grains subjected to temperature loading

Author:

Chyuan Shiang-Woei

Publisher

Elsevier BV

Subject

Applied Mathematics,Computer Graphics and Computer-Aided Design,General Engineering,Analysis

Reference25 articles.

1. Finite Elements and Approximation;Zienkiewicz,1983

2. Finite Element Procedures in Engineering Analysis;Bathe,1982

3. Predictive surveillance technique for air-launched rocket motors;Svob;J. Spacecr.,1984

4. K.W. Bills Jr., Structural design nomograph for thermal cycling of tactical rocket propellants, NWC Tech. Memo 3365, December 1977.

5. Shiang-Woei Chyuan, Life assessment of solid-propellant structure under thermal cycling (structure over test) using structural design nomograph, Proceedings of The Fifth ROC Symposium on Fracture Science, 1998, pp. 31–38 (in Chinese).

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