@techreport{oai:jaxa.repo.nii.ac.jp:00043539,
 author = {藤森, 俊郎 and 河合, 理文 and 安藤, 安則 and 大森, 保紀 and 麻生, 茂 and 福田, 正大 and Fujimori, Toshiro and Kawai, Masafumi and Ando, Yasunori and Oomori, Yasunori and Fukuda, Masahiro},
 month = {Dec},
 note = {Three-dimensional Reynolds-averaged full Navier-Stokes equation including chemical reactions solver is developed to predict flow fields in SCRAMjet engine combustors. Using the above code, sonic gas transverse injections behind the rearward-facing step into the M=3.7 supersonic flow are investigated numerically. The numerical results are compared with the result of the transverse injection on the flat plate. The comparison shows that mixing of injectant gas with main air flow is enhanced by the rearwardfacing step., 資料番号: NALSP0016043, レポート番号: NAL SP-16},
 title = {後ろ向きステップ後方からの超音速中への垂直噴射の数値解析},
 year = {1991}
}