@inproceedings{oai:jaxa.repo.nii.ac.jp:00003856,
 author = {齊藤, 健一 and 吉本, 周生 and Saitoh, Kenichi and Yoshimoto, Norio},
 book = {宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県, 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan, A validation of a CFD code for transonic unsteady flow is important to the aeroelastic design of an aircraft. The wind-tunnel test was performed at the Transonic Wind-tunnel Gottingen to measure the unsteady pressure distributions in the DLR - JAXA cooperative frame work. A two-dimensional wing which has NLR-7301 profile was excited in pitching and flap motion. The test results measured in the adaptive wall test cart ware compared with the NS analysis with free stream boundary condition. Higher harmonic component of the pressure distributions were also compared in this paper., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530023021, レポート番号: JAXA-SP-14-010},
 pages = {117--120},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {適合壁における二次元翼非定常空気力計測試験とその解析},
 volume = {JAXA-SP-14-010},
 year = {2015}
}