@inproceedings{oai:jaxa.repo.nii.ac.jp:00004117,
 author = {Mouton, Sylvain and Lyonnet, Marianne and LeSant, Yves},
 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, During wind tunnel tests, any aircraft model deforms as a result of aerodynamic loads. This behaviour is generally regarded as a spurious effect of the testing technique that needs to be accounted for and corrected. This paper presents available optical technique to measure wing deformation in ONERA wind tunnels, and introduces a simulation method to predict the effect of the deformation on the model aerodynamic characteristics., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062070009, レポート番号: JAXA-SP-13-001E},
 pages = {115--129},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Prediction of the Aerodynamic Effect of Model Deformation during Transonic Wind Tunnel Tests},
 volume = {JAXA-SP-13-001E},
 year = {2013}
}