@inproceedings{oai:jaxa.repo.nii.ac.jp:00014459,
 author = {植松, 太郎 and 石田, 拓郎 and 麻生, 茂 and 谷, 泰寛 and Uematsu, Taro and Ishida, Takuro and Aso, Shigeru and Tani, Yasuhiro},
 book = {宇宙航行の力学シンポジウム, Symposium on Flight Mechanics and Astrodynamics},
 month = {Dec},
 note = {宇宙航行の力学シンポジウム(平成20年度)(2008年12月4～5日、宇宙航空研究開発機構宇宙科学研究本部), Symposium on Flight Mechanics and Astrodynamics 2008 (December 4-5, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, In this paper, we focused on reduction of reflected shock wave generated between two bodies in hypersonic flow field. To investigate reflected shock wave, we conducted wind tunnel experiments using TSTO models; the one has a rounded nosed circular cylinder configuration, the other has slender body.The slender body has three cross section configuration types(circle, triangle and square). From the results, the slender body having triangle cross section configuration can have weakest reflected shock wave in three TSTO models., 資料番号: AA0064729036},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {TSTO型宇宙往還機の空中分離における空力干渉の低減},
 volume = {平成20年度},
 year = {2009}
}