@inproceedings{oai:jaxa.repo.nii.ac.jp:00006154,
 author = {山下, 博 and 米澤, 誠仁 and 後藤, 悠一郎 and 大林, 茂 and 楠瀬, 一洋 and Yamashita, Hiroshi and Yonezawa, Masahito and Goto, Yuichiro and Obayashi, Shigeru and Kusunose, Kazuhiro},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2005論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2005},
 month = {Feb},
 note = {Although many kinds of aircrafts are produced, until now, the Concorde is the only supersonic commercial transport (SST) ever built. However, it made its final flight in 2003. It is everyone's dream to be able to go anywhere faster and at the same time ensuring comfort. One of the fundamental problems preventing commercial transport from going supersonic is the creation of strong sonic boom by shock waves. Here we propose a new concept of 'Biplane'. This concept is practical for achieving boomless supersonic aircraft. The aim of this research is to study the shock wave behaviors of Busemann's Biplane for a wide range of Mach numbers and angle of attack, using CFD (Computational Fluid Dynamics) code in inviscid flow (Euler) mode. As the results, the CFD analyses capture a choked flow phenomenon of Busemann's Biplane., 資料番号: AA0049212021, レポート番号: JAXA-SP-05-017},
 pages = {126--131},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {超音速2枚翼型における衝撃波のCFD解析},
 volume = {JAXA-SP-05-017},
 year = {2006}
}