@inproceedings{oai:jaxa.repo.nii.ac.jp:00036751,
 author = {Chue, R.S.M. and 伊藤, 勝宏 and Chue, Randy S. M. and Ito, Katsuhiro},
 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 8 Jun. 1995 東京 日本, National Aerospace Laboratory 8 Jun. 1995 Tokyo Japan, 高エンタルピー反射型衝撃風洞中の駆動気体汚染を調べるために数値計算を行った。この研究は反射衝撃波と壁面境界層および接触面インターフェースの相互作用、および駆動気体汚染に対するそれらの寄与のような非定常事象に焦点を当てた。最適および非最適風洞作動条件やチョークノズルの効果についても論じた。, A computational study has been carried out to examination in a high-enthalpy reflected shock tunnel. The investigation focused on the nonsteady events as the reflected shock interacts with the wall boundary layer and the contact interface and their contribution to driver gas contamination. Both tailored and off-tailored tunnel operating conditions and the effects of a choked nozzle are discussed in the present paper., 資料番号: AA0000110001, レポート番号: NAL SP-29},
 pages = {3--9},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {A computational study of driver gas contamination in a high enthalpy shock tunnel},
 volume = {29},
 year = {1996}
}