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2. 2) Matsushima, K., Iwamiya, T. and Ishikawa, H.: Supersonic Inverse Design of Wings for the Full Configuration of Japanese SST, Proceedings of the 22nd ICAS Congress, ICAS 2000 Congress, 2000, pp. 213.1–213.8.
3. 3) Boeing Company web page: http://www.boeing.com/
4. 4) Haines, B.: The Aerodynamic Design of the Wing-Fuselage for a Near-Sonic Transport, AIAA Paper 2002-0517, 2002.
5. 5) Takenaka, K., Nakao, M., Yamamoto, K. and Takaki, R.: NEXST-1の音速近傍流れ場解析とその検証，第16回数値流体力学シンポジウム講演論文集，2002, C13-4.