@inproceedings{oai:jaxa.repo.nii.ac.jp:00005790,
 author = {越智, 章生 and 嶋, 英志 and Ochi, Akio and Shima, Eiji},
 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ワークショップ.次世代超音速機の数値シミュレーション利用技術に関する国際ワークショップ 航空宇宙技術研究所 20011203-20011205 東京 日本, SST-CFD Workshop. International Workshops on Numerical Simulation Technology for Design of Next Generation Supersonic Civil Transport National Aerospace Laboratory 20011203-20011205 Tokyo Japan, This paper provides CFD (Computational Fluid Dynamics) flow analysis results of the NAL NEXST-1 (National EXperimental Supersonic Transport-1) for the 3rd NAL SST (SuperSonic Transport) CFD workshop. A hybrid unstructured grid system was employed for viscous aerodynamic analysis. Computations were conducted for both wind tunnel test condition and Flight Test condition. The CFD results showed very good correlation with wind tunnel test results., 資料番号: AA0063609059, レポート番号: JAXA-SP-06-029E},
 pages = {474--477},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {A flow analysis of the NAL NEXST-1 using hybrid unstructured grid system},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}