@inproceedings{oai:jaxa.repo.nii.ac.jp:00038088,
 author = {牧田, 光正 and 林, 茂 and 川名, 輝子 and 筧, 雅行 and 小池, 秀耀 and 小林, 敏雄 and 谷口, 伸行 and Makida, Mitsumasa and Hayashi, Shigeru and Kawana, Teruko and Kakei, Masayuki and Koike, Hideaki and Kobayashi, Toshio and Taniguchi, Nobuyuki},
 book = {航空宇宙技術研究所特別資料: 航空宇宙数値シミュレーション技術シンポジウム2001論文集, Special Publication of National Aerospace Laboratory: Proceedings of Aerospace Numerical Simulation Symposium 2001},
 month = {Jan},
 note = {A turbulent combustion analysis code is being developed for large scale numerical simulation of combustion phenomena using parallel computing machines. In this study the following calculations were made. Firstly, zero Mach number approximation is applied to the analysis of subsonic compressible flow, and BFC coordinate is taken for considering the real complicated shape of the burner. Secondly, the stabilization of the simulation including various time scales is realized by coupling equation of continuity with equation of energy conservation via equation of state. The result of LES simulation shows that it is qualitatively valid for the real combustion phenomena., 資料番号: AA0032819052, レポート番号: NAL SP-53},
 pages = {303--308},
 publisher = {航空宇宙技術研究所, National Aerospace Laboratory (NAL)},
 title = {並列計算機による時間変動成分を考慮した乱流燃焼解析ソフトウェアの開発:2次元予混合火炎バーナーの解析},
 volume = {53},
 year = {2002}
}