@techreport{oai:jaxa.repo.nii.ac.jp:00041339,
 author = {Timofeev, Eugene and Voinovich, Peter and 高山, 和喜 and Molder, Sannu and Studzienny, Arthur and Alinejad, Maziar and Timofeev, Eugene and Voinovich, Peter and Takayama, Kazuyoshi and Molder, Sannu and Studzienny, Arthur and Alinejad, Maziar},
 month = {Dec},
 note = {航空宇宙技術研究所 7-9 Jun. 2000 東京 日本, National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan, 本論文では、以前開発した本質的に非定常的な衝撃波流のための部分適応型非構造数値コードを吸気口始動過程のシミュレーションに応用した、最近の取り組みについて概説し、その可能性を説明した。2次元および3次元吸気口についての結果を示した。, The present paper outlines the recent activities on the application of previously developed locally adaptive unstructured numerical codes for essentially unsteady shocked flows to the simulation of inlet starting process and demonstrates their possibilities. Results for 2D (two dimensional) and 3D (three dimensional) inlets are presented., 資料番号: AA0028635038, レポート番号: NAL SP-46},
 title = {Numerical methods to simulate 2D and 3D inlet starting},
 year = {2000}
}