@inproceedings{oai:jaxa.repo.nii.ac.jp:00004120,
 author = {村山, 光宏 and 横川, 譲 and 山本, 一臣 and 伊藤, 靖 and 雨宮, 和久 and 田中, 健太郎 and 平井, 亨 and Murayama, Mitsuhiro and Yokokawa, Yuzuru and Yamamoto, Kazuomi and Ito, Yasushi and Amemiya, Kazuhisa and Tanaka, Kentaro and Hirai, Tohru},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication},
 month = {Nov},
 note = {5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan, In this paper, computational efforts in designing experiment for a series of wind tunnel tests of high- lift airframe noise measurement and the importance are shown. This paper describes computational evaluations of the design of wind tunnel testing model, the model sizing and mounting in wind tunnel, and influences of shear layer and mounted plate on the sound propagation in open-cart test section. It is shown that preliminary CFD investigation of the wind tunnel tests can decrease unknowns and improve the accuracy of the wind tunnel test., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062070012, レポート番号: JAXA-SP-13-001E},
 pages = {167--182},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Computational Efforts in Designing Experiment for High-lift Aeroacoustics},
 volume = {JAXA-SP-13-001E},
 year = {2013}
}