@inproceedings{oai:jaxa.repo.nii.ac.jp:00038043,
 author = {山本, 行光 and 穂積, 弘一 and 津田, 尚一 and 小山, 忠勇 and 平林, 則明 and Yamamoto, Yukimitsu and Hozumi, Koichi and Tsuda, Shoichi and Koyama, Tadao and Hirabayashi, Noriaki},
 book = {航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001},
 month = {Jan},
 note = {Hypersonic aerodynamic interactions for two hemisphere-cylinders have been investigated numerically and experimentally for future TSTO space transport problems. Two hemisphere models with a diameter of 3 cm and 6 cm are placed parallel or with the inclined angle from 13 to 16 deg and complicated shock-shock interactions which generates severe heating on the body surface are studied by using NAL Mach 10 Hypersonic Wind Tunnel and CFD analysis. The purpose of the present study is to understand the complicated flow phenomena and to predict the related severe peak heating rate in the interaction area. Finally, proposals of CFD workshop are made for these two body shock/shock interaction problems. These works contribute to future TSTO aerodynamic design problems in both cruising and separation stages., 資料番号: AA0032819007, レポート番号: NAL SP-53},
 pages = {35--41},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {TSTO2体問題衝撃波干渉加熱と検証課題の提案},
 volume = {53},
 year = {2002}
}