Numerical Analysis on Flight-Test Results of Supersonic Experimental Airplane NEXST-1
Author:
Affiliation:
1. Sankosoft Company, Ltd., Shinjuku, Tokyo 169-0075, Japan
2. Japan Aerospace Exploration Agency, Mitaka, Tokyo 181-0015, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.33595
Reference16 articles.
1. Flight Test Measurements of Surface Pressure on Unmanned Scaled Supersonic Experimental Airplane
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