@inproceedings{oai:jaxa.repo.nii.ac.jp:00003647,
 author = {藤田, 和央 and 小澤, 宇志 and 高桝, 大樹 and 松山, 新吾 and 滝沢, 直美 and Fujita, Kazuhisa and Ozawa, Takashi and Takayanagi, Hiroki and Matsuyama, Shingo and Takizawa, Naomi},
 book = {宇宙航空研究開発機構特別資料: 第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 47th Fluid Dynamics Conference / the 33rd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学生産技術研究所), 目黒区, 東京, 47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (July 2-3, 2015. Institute of Industrial Science , the University of Tokyo), Meguro-ku, Tokyo, Japan, Comprehensive challenges toward development of aerodynamic database for Mars exploration aeroshell are overviewed. Direct Simulation Monte-Carlo (DSMC) computations of rarefied flows around the Martian entry system and direct force measurements of the model in the hypersonic rarefied wind-tunnel are conducted to determine the rarefied aerodynamics of the aeroshell. Hypersonic, supersonic, and transonic aerodynamic performance of the aeroshell are investigated by corresponding wind-tunnel tests, with the aid of computational-fluid-dynamic (CFD) computations. Investigations on the front aeroshell separation dynamics are conducted as well., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1630005022, レポート番号: JAXA-SP-15-013},
 pages = {145--146},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {火星探査機のエアロシェル空力データベース開発に向けて},
 volume = {JAXA-SP-15-013},
 year = {2016}
}