@inproceedings{oai:jaxa.repo.nii.ac.jp:00004115,
 author = {HantraisGervois, Jean-Luc and Piat, Jean-Francois},
 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, This paper presents a methodology to estimate the wind tunnel wall interference with RANS simulations. The method involves a pairing process between confined and aerodynamically equivalent free air simulations that is carried out through automatic optimisation. Wall corrections are derived for a major industrial wind tunnel (ONERA S2MA wind tunnel located in Modane). The tunnel is a transonic pressurised tunnel with perforated walls that can be sealed to achieve a guided test section. In order to model the porous walls in the RANS simulations, the characteristics of the walls were measured with a specific experiment.On the whole, in the linear aerodynamic domain, the RANS corrections are similar to the current correction strategy but require a higher CPU cost. The benefit appears in non-linear regimes (high lift or high Mach number)., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062070007, レポート番号: JAXA-SP-13-001E},
 pages = {83--102},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {A Methodology to Derive Wind Tunnel Wall Corrections from RANS Simulations},
 volume = {JAXA-SP-13-001E},
 year = {2013}
}