@inproceedings{oai:jaxa.repo.nii.ac.jp:00014703,
 author = {瀬崎, 新士 and 中村, 弘明 and 西尾, 正富 and Sezaki, Shinji and Nakamura, Hiroaki and Nishio, Masatomi},
 book = {宇宙航行の力学シンポジウム　平成14年度, Symposium on Flight Mechanics and Astrodynamics 2002},
 month = {Mar},
 note = {In this study, the flowfield around future TSTO Launch Vehicle was investigated by utilizing an electric discharge method. The experiments were carried out under the condition that the angles of attack of the model are -10, 0, and 10 deg. Shock shapes around a model were visualized. These results confirmed that discontinuous planes of density change existed in the shock-layer. The structures of shock waves and discontinuous planes of density change were shown in this paper. When angles of attack of the model became large, there was a tendency for the thickness of each layer to become thin., 資料番号: AA0045913016},
 pages = {59--62},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {将来型TSTO宇宙往還機周りの流れ場の研究},
 year = {2003}
}