@inproceedings{oai:jaxa.repo.nii.ac.jp:00005776,
 author = {二ツ寺, 直樹 and 海田, 武司 and Futatsudera, Naoki and Kaiden, Takeshi},
 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, In 1997, National Aerospace Laboratory (NAL) started a program to develop a scaled supersonic experimental airplane to establish the technological basis for the development of the next generation supersonic transport. A non-powered experimental airplane is being developed for the first experimental flight in 2002. The airplane is launched by a rocket-booster. After the rocket-booster is separated, the airplane starts the measurement flight at Mach 2.0 and altitude 18.5 km. In the aerodynamic design of the experimental airplane, Mitsubishi Heavy Industries, Ltd. (MHI) is in charge of the overall design and NAL mainly conducted the wing and wing-body aerodynamic integration design with their sophisticated CFD (Computational Fluid Dynamics) code. MHI is also in charge of the launch configuration aerodynamic design. In the MHI design work, wind tunnel test data were mainly used. Some experimental data were checked and corrected using the CFD analysis. CFD analysis also played an important role in understanding physical phenomena of the complicated flow field of the experimental airplane and the rocket-booster., 資料番号: AA0063609045, レポート番号: JAXA-SP-06-029E},
 pages = {380--389},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Some practical applications of CFD analysis to aerodynamic design of the supersonic experimental airplane},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}