@inproceedings{oai:jaxa.repo.nii.ac.jp:00037333,
 author = {嶋田, 徹 and 山本, 行光 and 廣瀬, 直喜 and Shimada, Toru and Yamamoto, Yukimitsu and Hirose, Naoki},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Feb},
 note = {航空宇宙技術研究所 24-26 Jun. 1998 東京 日本, National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan, HYFLEX(極超音速飛行実験)に関するHEK(角田宇宙推進技術研究センター高温衝撃風洞)風試結果を評価する目的で、3次元熱化学非平衡流れの数値解析を実施し、解析結果を風試結果および既存の相関と比較した。計算結果は相関式とおおむね一致する結果を得たが、試験結果に比べると若干低めの値を示した。, Numerical simulations of three dimensional thermochemical nonequilibrium flow around HYFLEX (Hypersonic Flight Experiment) reentry vehicle have been conducted to evaluate heat flux measurement in HEK (High Enthalpy shock tunnel at Kakuda Research Center) ground tests. Computed results are compared with the experiment as well as existing correlation. The computed results agree well with the correlation, but fell short of the measured data., 資料番号: AA0001958019, レポート番号: NAL SP-41},
 pages = {123--128},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {再突入機の周りの3次元高エンタルピー流れの数値シミュレーション},
 volume = {41},
 year = {1999}
}