@inproceedings{oai:jaxa.repo.nii.ac.jp:00038041,
 author = {坂元, 康朗 and 辻本, 健士 and Sakamoto, Yasuro and Tsujimoto, Takeshi},
 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 = {In this paper, some results of hypersonic CFD simulation of HOPE-X vehicle by commercial CFD code 'INCA', which are available for non-equilibrium flow analysis to estimate real gas effect at reentry phase, is presented. Compared with the results by NAL code and wind tunnel, it appears that the commercial CFD solver enables to take some suitable results, so that it is to confirm the tool's potential and the step to define the aerodynamic characteristics in HOPE-X design., 資料番号: AA0032819005, レポート番号: NAL SP-53},
 pages = {25--28},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {市販コードINCAを用いたHOPE-Xまわりの極超音速流CFD解析},
 volume = {53},
 year = {2002}
}