@inproceedings{oai:jaxa.repo.nii.ac.jp:00005765,
 author = {大庭, 芳則 and 児玉, 秀和 and 野崎, 理 and 菊地, 一雄 and 西澤, 敏雄 and 松尾, 裕一 and Oba, Yoshinori and Kodama, Hidekazu and Nozaki, Osamu and Kikuchi, Kazuo and Nishizawa, Toshio and Matsuo, Yuichi},
 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, The SST (SuperSonic Transport) propulsion system will operate in the range from takeoff to high Mach number. The high speed flight causes very high inlet air temperatures and pressures and the high inlet air temperatures and recovery pressures inside the engine make cooling for elements of the engine mandatory to keep the best available construction materials operating satisfactorily. Technology for satisfied cooling requires to understand the heat transfer in the engine, however there are many difficulties to understand detailed phenomena occurred in the engine from limited measurement. This paper describes some CFD (Computational Fluid Dynamics) applications for a SST propulsion system which were carried to understand the mechanisms of flowfields and heat transfer in the engine., 資料番号: AA0063609034, レポート番号: JAXA-SP-06-029E},
 pages = {304--309},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {CFD application to SST propulsion system},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}