Flow Simulation of an Supersonic Transport Configuration at Low-Speed and High-Lift Conditions
Author:
Affiliation:
1. Japan Aerospace Exploration Agency, Tokyo 181-0015, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.33856
Reference15 articles.
1. HSCT high-lift aerodynamic technology requirements
2. European research to reduce drag for supersonic transport aircraft
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