@inproceedings{oai:jaxa.repo.nii.ac.jp:00006470,
 author = {渡辺, 重哉 and 加藤, 裕之 and Lei, Zhong and 今村, 太郎 and 榎本, 俊治 and Watanabe, Shigeya and Kato, Hiroyuki and Lei, Zhong and Imamura, Taro and Enomoto, Shunji},
 book = {宇宙航空研究開発機構特別資料: 航空宇宙数値シミュレーション技術シンポジウム2004論文集, JAXA Special Publication: Proceedings of Aerospace Numerical Simulation Symposium 2004},
 month = {Mar},
 note = {Possibilities of Particle Image Velocimetry (PIV) as a tool to acquire detailed experimental data for unsteady CFD code validation are discussed. Two examples of PIV data compared with corresponding CFD data, that is, leading edge separation vortices of a cranked arrow wing and a tip vortex of a rectangular wing, are presented in order to evaluate the capability of PIV as a CFD validation tool. As a result, the detailed velocity field data via PIV are proved to be useful in the evaluations of different turbulence models and algorithms in CFD analyses. Also, important issues to be carefully considered for getting successful results in the CFD validation using PIV are mentioned, such as differences in spatial/temporal resolutions and data point locations., 資料番号: AA0048469030, レポート番号: JAXA-SP-04-012},
 pages = {178--183},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {PIV(粒子画像流速測定法)を用いたCFDコード検証について},
 volume = {JAXA-SP-04-012},
 year = {2005}
}