@inproceedings{oai:jaxa.repo.nii.ac.jp:00005763,
 author = {松島, 紀佐 and 岩宮, 敏幸 and Zhang, Wanqiu and Matsushima, Kisa and Iwamiya, Toshiyuki and Zhang, Wanqiu},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)},
 month = {Mar},
 note = {SST-CFDワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20000117-20000119 東京 日本, SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20000117-20000119 Tokyo Japan, Aerodynamic shape of a wing for NAL (National Aerospace Laboratory)'s first SST (SuperSonic Transport) model has been designed by a supersonic inverse design method. This method handles wing-fuselage configurations and provides wing section's geometry at every span for Navier-Stokes flowfields. The design target is a NLF (Natural Laminar Flow) wing at the speed of M(sub infinity) = 2.0. The original system of the inverse design method has to be modified so that several design constraints can be satisfied. By means of the method, a wing section shape which has much more desirable characteristics has been designed than that by the traditional design method. In terms of aerodynamics to realize a NLF wing, the modified method works very well. The pressure distribution of the designed wing shows good agreement with the target pressure. In terms of constraints, most of them can be satisfied by using the modified design method; however, difficulty has been found during the process for thickness constraint control. The prospective strategy to cope with the thickness constraint is discussed., 資料番号: AA0063609032, レポート番号: JAXA-SP-06-029E},
 pages = {286--291},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Inverse wing design for the scaled supersonic experimental airplane with ensuring design constraints},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}