Computational Fluid Dynamics Evaluation of National Aerospace Laboratory Experimental Supersonic Airplane in Ascent
- 1 March 2002
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 39 (2), 359-364
- https://doi.org/10.2514/2.2935
Abstract
No abstract availableKeywords
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