@inproceedings{oai:jaxa.repo.nii.ac.jp:00005737,
 author = {中村, 佳朗 and Lahur, Paulus R. and 林, 大雄 and Nakamura, Yoshiaki and Lahur, Paulus R. and Hayashi, Daiyu},
 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 simple model was proposed to predict the transition region of compressible flow. An algebraic type of RNG (Renormalization Group) model was employed with modified expressions for dissipation rate and length-scale. A 2D flat plate flow with no pressure gradient was calculated to validate the model. The results showed favorable agreement with theoretical values, which suggests its capability to predict the transition cases for simple flow., 資料番号: AA0063609006, レポート番号: JAXA-SP-06-029E},
 pages = {39--43},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {A transition prediction model in supersonic flow},
 volume = {JAXA-SP-06-029E},
 year = {2007}
}