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タイトルComparison of Measured and Block Structured Simulations for the F-16XL Aircraft
本文(外部サイト)http://hdl.handle.net/2060/20090014739
著者(英)Massey, S. J.; Abdol-Hamid, K. S.; Badcock, K. J.; Elmilgui, A.; Boelens, O. J.
著者所属(英)NASA Langley Research Center
発行日2008-01-01
言語eng
内容記述This article presents a comparison of the predictions of three RANS codes for flight conditions of the F-16XL aircraft which feature vortical flow. The three codes, ENSOLV, PMB and PAB3D, solve on structured multi-block grids. Flight data for comparison was available in the form of surface pressures, skin friction, boundary layer data and photographs of tufts. The three codes provided predictions which were consistent with expectations based on the turbulence modelling used, which was k- , k- with vortex corrections and an Algebraic Stress Model. The agreement with flight data was good, with the exception of the outer wing primary vortex strength. The confidence in the application of the CFD codes to complex fighter configurations increased significantly through this study.
NASA分類Aircraft Design, Testing and Performance
レポートNOLF99-6825
権利Copyright, Distribution as joint owner in the copyright


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