@inproceedings{oai:jaxa.repo.nii.ac.jp:00037872,
 author = {高倉, 葉子 and 小川, 哲 and Takakura, Yoko and Ogawa, Satoru},
 book = {航空宇宙技術研究所特別資料, Special Publication of National Aerospace Laboratory},
 month = {Dec},
 note = {数値計算の信頼性を調べる目的で、航空宇宙技術研究所遷音速風洞内のONERA-M5全機形状模型のまわりの流れを数値的に解析する試みを続けている。この試みでは、複雑な形状のまわりの流れの計算を行うために領域分割法を用い、各部分領域でChakravathy-OsherのTVDスキームにより薄層近似ナビエ･ストークス方程式を解いている。今回は、航空宇宙技術研究所並列ベクトル計算機NWT上におけるこの領域分割法の単純ベクトル並列アルゴリズムを示し、それによるシミュレーションを行う。計算された圧力、揚力および抵抗は実験値とよく一致した。並列処理の性能に関しては、計算時間が最大の格子点数をもつ部分領域上の計算時間にまで短縮され、要素プロセッサ間の交信所要時間は無視し得るほどに小さい。, It has been tried continuously to numerically analyze NAL (National Aerospace Laboratory) transonic wind-tunnel flows about a fully configured model of aircraft, ONERA-M5, to investigate the reliability of numerical computations; in these trials a multi-domain technique is used to realize the computations of flows about a complicated configuration, and in each domain thin-layer Navier-Stokes equations are solved by the Chakravarthy-Osher TVD (Total Variation Diminishing) scheme. In this time the simple vector-parallel algorithm of this multi-domain technique on NAL's Numerical Wind Tunnel (NWT) system is presented and simulations have been performed. Consequently the computed pressure, lift and drag coefficients have agreed well with experimental ones. Regarding the parallel performance, the parallel-computing time has been reduced to the computing time on the domain with the largest number of grid points, and communication time between Processor Elements (PEs) can be negligible., 資料番号: AA0004174035, レポート番号: NAL SP-27},
 pages = {243--248},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {遷音速風洞内全機模型流れのベクトル･パラレル･シミュレーション},
 volume = {27},
 year = {1994}
}