@inproceedings{oai:jaxa.repo.nii.ac.jp:00005792,
 author = {近藤, 匡泰 and Yang, Guowei and 大林, 茂 and Kondo, Masahiro and Yang, Guowei and Obayashi, Shigeru},
 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, An implicit multiblock Navier-Stokes solver, which contains the LU-SGS (Lower-Upper Symmetric Gauss-Seidel) subiteration method and the HLLEW (Harten-Lax-van Leer Einfeldt-Wada) scheme, has been developed for numerical simulations on complex and realistic aerodynamic configurations. One-level halo cells are used to communicate data between abutting blocks. The resulting method is applied to the NAL SuperSonic Transport (SST) model., 資料番号: AA0063609061, レポート番号: JAXA-SP-06-029E},
 pages = {484--485},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {Multiblock Navier-Stokes solver for SST wing-fuselage configuration},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}