@inproceedings{oai:jaxa.repo.nii.ac.jp:00036870,
 author = {山本, 行光 and Yamamoto, Yukimitsu},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Jan},
 note = {航空宇宙技術研究所 6-7 JUN. 1996 東京 日本, National Aerospace Laboratory 6-7 JUN. 1996 Tokyo Japan, NAL-M10-HWT(極超音速風洞)、ONERA-S4MA-HWT、Calspans衝撃波トンネル、Caltech-T-5高エンタルピー衝撃波トンネルなどを含む極超音速風洞実験と極超音速CFD(数値流体力学)解析との最近の比較を紹介した。また、OREX(軌道再突入実験機)およびHYFLEX(極超音速飛行実験)などの極超音速再突入飛行解析を行った。これらの研究を通し、再突入機体の熱空力加熱特性を詳細に検討した。, Recent comparisons of hypersonic CFD (Computational Fluid Dynamics) analysis with hypersonic wind tunnel experiments, including NAL M10 HWT (Hypersonic Wind Tunnel), ONERA S4MA HWT, Calspan's shock tunnel and Caltech T-5 high enthalpy shock tunnel, are introduced. Also, hypersonic reentry flight analysis, such as OREX (Orbital Reentry Experiment) and HYFLEX (Hypersonic Flight Experiment) are made. Through these studies, aerothermodynamic heating characteristics of reentry vehicle are investigated in detail., 資料番号: AA0000685011, レポート番号: NAL SP-34},
 pages = {55--60},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {再突入飛行体まわりの空力加熱のCFD解析と実験},
 volume = {34},
 year = {1997}
}