Structurally compliant rocket engine combustion chamber - Experimental and analytical validation
Author:
Affiliation:
1. NASA Lewis Research Center, Cleveland, Ohio 44135
2. University of Akron, Akron, Ohio 44325
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26665
Reference17 articles.
1. Finite element implementation of Robinson's unified viscoplastic model and its application to some uniaxial and multiaxial problems
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