Validation of global aeropropulsive characteristics of integrated configurations
Author:
Affiliation:
1. Dassault Aviation, St.-Cloud, France
2. RAS, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1998-1624
Reference8 articles.
1. Hypersonic airbreathing aircraft integration through CFD - Global simulations for global thinking
2. Symmetrization of conservation laws with entropy for high-temperature hypersonic computations
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