@inproceedings{oai:jaxa.repo.nii.ac.jp:00006167,
 author = {坪井, 伸幸 and 宮路, 幸二 and 藤田, 和央 and 澤井, 秀次郎 and 小林, 弘明 and 小島, 孝之 and 山川, 宏 and 橋本, 樹明 and Tsuboi, Nobuyuki and Miyaji, Koji and Fujita, Kazuo and Sawai, Shujiro and Kobayashi, Hiroaki and Kojima, Takayuki and Yamakawa, Hiroshi and Hashimoto, Tatsuaki},
 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2005論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005},
 month = {Feb},
 note = {Development of Balloon-based Operation Vehicle (BOV) is currently in progress for the first flight scheduled in 2006. A vehicle in a wing-body configuration will be lifted by a high-altitude balloon and dropped. Various types of onboard experiments such as a microgravity experiment and a demonstration of a supersonic engine are planned during flights for the second, third and fourth flights. The aerodynamics load and characteristics of BOVs have been obtained by the CFD simulations as well as by the wind tunnel testing in ISAS. In this paper, the numerical simulations for BOV are presented and the results showed that the interaction between the wings, body and engine increases for transonic flow with high angle of attack., 資料番号: AA0049212034, レポート番号: JAXA-SP-05-017},
 pages = {203--208},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {微小重力実験機の空力特性に関する数値シミュレーション},
 volume = {JAXA-SP-05-017},
 year = {2006}
}