Supersonic/Hypersonic Euler Flowfield Prediction Method for Aircraft Configurations
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/5.9781600865985.0839.0861
Reference79 articles.
1. ^erhoff, A., and O'Neil, P. J. "A Natural Formulation for Numerical Solution of the Euler Equations," AIAA Paper 84-0163, Jan.1984.
2. Accurate, efficient prediction method for supersonic/hypersonic inviscid flow
3. 4Agrawal, S., Vermeland, R., Verhoff, A., and Lowrie, R. B. "Euler Transonic Solutions over Finite Wings," AIAA Paper 88-0009, Jan.1988.
4. Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodies
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