@inproceedings{oai:jaxa.repo.nii.ac.jp:00004143,
 author = {原, 達矢 and 沼田, 大樹 and 浅井, 圭介 and 伊藤, 崇文 and 姜, 欣 and Hara, Tatsuya and Numata, Daiju and Asai, Keisuke and Ito, Takafumi and Jiang, Xin},
 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, The purpose of this study is to measure the unsteady force acting on a slender delta wing in two degree-of-freedom (DoF) motion. A serial-type robot manipulator was used to oscillate the model in two modes; one is roll-yaw coupled lateral motion and the other is pitch-heave coupled longitudinal motion. Unsteady forces and moments were measured by a six-component balance and the effects of oscillation frequency and amplitude were evaluated. In the 2-DoF roll-yaw coupled mode, hysteresis loop was noted at high angles of attack and changes of rolling moment are delayed as compared with the 1-DoF case. In the pitch-heave coupled experiment, it was found that the effect of pitch rate on unsteady force is negligible at the frequency and amplitude ranges covered in this experiment., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062070035, レポート番号: JAXA-SP-13-001E},
 pages = {397--405},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Dynamic Wind-Tunnel Testing of a Delta Wing Using a Multi-Degree-of-Freedom Robotic Manipulator},
 volume = {JAXA-SP-13-001E},
 year = {2013}
}