Numerical simulation of the dynamic thermostructural response of a composite rocket nozzle throat

Author:

Morozov E.V.,de la Beaujardiere J.F.P. Pitot

Publisher

Elsevier BV

Subject

Civil and Structural Engineering,Ceramics and Composites

Reference9 articles.

1. Thermostructural analysis of rotationally symmetric multidirectional fibrous composite structures;Mukherjee;Comput Struct,1997

2. Vandenboom M, Heister SD. Application of advanced materials in a composite rocket nozzle. In: Proceedings of 34th AIAA/ASME/SAE/ASEE joint propulsion conference and exhibit. Cleveland, USA; 1998.

3. Cozart AB, Shivakumar KN. Stress analysis of a 3-D braided composite ablative nozzle. In: Proceedings of 40th AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials conference and exhibit, AIAA/ASME/AHS adaptive structures forum and AIAA forum on non-deterministic approaches. St. Louis, USA; 1999.

4. Thermoelastic analysis of a kick motor nozzle incorporating spatially reinforced composites;Yoo;J Spacecraft Rocket,2003

5. Thermo-structural analysis of composite structures;Kumar;Mater Sci Eng,2005

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