@inproceedings{oai:jaxa.repo.nii.ac.jp:00005751,
 author = {平井, 健二 and 児玉, 秀和 and 野崎, 理 and 菊地, 一雄 and 西澤, 敏雄 and 田村, 敦宏 and 松尾, 裕一 and Hirai, Kenji and Kodama, Hidekazu and Nozaki, Osamu and Kikuchi, Kazuo and Nishizawa, Toshio and Tamura, Atsuhiro and Matsuo, Yuichi},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport (SST-CFD Workshop)},
 month = {Mar},
 note = {SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design 航空宇宙技術研究所 19980316-19980317 東京 日本, SST-CFD Workshop. International CFD Workshops for Super-sonic Transport Design National Aerospace Laboratory 19980316-19980317 Tokyo Japan, A three-dimensional time-accurate Reynolds-averaged Navier-Stokes code has been extended for use in a parallel supercomputer called Numerical Wind Tunnel (NWT) developed by the Japanese National Aerospace Laboratory. The power of parallel supercomputer enables us to perform a more accurate computation of the unsteady flowfield within a multipassage configuration. The numerical simulations was aimed at investigating the unsteady flow behavior for a transonic fan rotor blade with inlet total pressure distortion, which is inclined to appear in a SST (SuperSonic Transport) propulsion system., 資料番号: AA0063609020, レポート番号: JAXA-SP-06-029E},
 pages = {180--183},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Unsteady flow analysis of fan rotor with inlet distortion},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}