@inproceedings{oai:jaxa.repo.nii.ac.jp:00006455,
 author = {浅野, 宏佳 and 越智, 章生 and 井上, 隆 and Asano, Hiroyoshi and Ochi, Akio and Inoue, Takashi},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004},
 month = {Mar},
 note = {JADC is conducting High Speed Transport Program (HSTP) aiming for the development of next generation high speed aircraft such as supersonic and transonic speed transport. In the FY2003, the aerodynamic design of high lift device as a part of this program were performed. This paper describes the optimum design of high lift device to improve the lift-to-drag ratio (L/D). The optimization process is based on the response surface method, where the effects of flaps are estimated by linear superposition. Navier-Stokes calculations are performed for the model either with leading-edge flaps or with trailing-edge flaps. Then the performance of the model with all flaps deflected is predicted by adding the effect of leading-edge flap and that of trailing-edge flap. The response surface is created for search of optimum value. This method reduces the computational time required for CFD analysis. Results of Navier-Stokes calculation for the optimum configuration indicate that the present method yields reasonable results., 資料番号: AA0048469015, レポート番号: JAXA-SP-04-012},
 pages = {93--98},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {超高速輸送機形状の高揚力装置の空力設計},
 volume = {JAXA-SP-04-012},
 year = {2005}
}