Aerodynamic Optimization of NEXST-1 SST Model at Near-Sonic Regime
Author:
Affiliation:
1. Tohoku University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-34
Reference21 articles.
1. Sakata, K.: Supersonic Experimental Airplane (NEXST) for Next Generation SST Technology, AIAAPaper2002-0527,2002.
2. Haines, B.: The Aerodynamic Design of the Wing-Fuselage for a Near-Sonic Transport- Early Thoughts and Results Revisited, AIAA Paper 2002-0517,2002.
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