@inproceedings{oai:jaxa.repo.nii.ac.jp:00004406,
 author = {中北, 和之 and 今川, 健太郎 and 高間, 良樹 and 加藤, 裕之 and 中島, 努 and Nakakita, Kazuyuki and Imagawa, Kentaro and Takama, Yoshiki and Kato, Hiroyuki and Nakajima, Tsutomu},
 book = {宇宙航空研究開発機構特別資料: 第43回流体力学講演会: 航空宇宙数値シミュレーション技術シンポジウム2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, Unsteady Pressure-Sensitive Paint (PSP) measurement of a rocket fairing model was conducted at the JAXA 2m x 2m Transonic Wind Tunnel as a part of the campaign to investigate the steady and unsteady flow field around it and to obtain the CFD validation data. Anodized-aluminum PSP was coated on the model surface, and it was illuminated using a high-power blue laser diode. AA-PSP luminescence was measured by a high-speed camera, whose frame rate was 5kfps. The high-speed camera images were calculated to the Cp data using in-situ PSP calibration. Unsteady PSP data captured unsteady pressure data on the rocket fairing model as time-series Cp images. The unsteady phenomena on the model were significantly varied according to the Mach number and the angle of attack. Frequency analysis was also applied to the time-series Cp data. Unsteady pressure distribution was clearly investigated from the power spectrum results., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207034, レポート番号: JAXA-SP-11-015},
 pages = {195--200},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ロケットフェアリング模型の非定常PSP計測},
 volume = {JAXA-SP-11-015},
 year = {2012}
}