论文信息 - Computational Simulation of a Semispan Wing in a Wind Tunnel

Computational Simulation of a Semispan Wing in a Wind Tunnel

The computational simulation of wind tunnel tests are central in efforts to improve the accuracy and range of applicability of CFD codes. A validation experiment in solid wall transonic wind tunnel is simulated with the inviscid and viscous tunnel wall computation models. Viscous wall modeling appears to provide the ability to reproduce the experimental conditions fairly well without wall interference corrections but specification of the actual wall geometry is crucial.

Michael E. Olsen | Yehia Rizkf

[1] Unver Kaynak,et al. Numerical simulation of transonic separated flows over low-aspect-ratio wings , 1987 .

[2] Terry L. Holst,et al. CFD validation for aerodynamic flows - Challenge for the '90's , 1990 .

[3] Veer N. Vatsa,et al. Effect of sidewall boundary layer on a wing in a wind tunnel , 1989 .

[4] Scott D. Thomas,et al. Numerical solution of transonic wing flowfields , 1982 .

[5] Joseph G. Marvin,et al. Accuracy requirements and benchmark experiments for CFD validation , 1988 .

[6] T. E. Polek,et al. A new facility and technique for two-dimensional aerodynamic testing , 1982 .

[7] Pieter G. Buning,et al. User's manual for the HYPGEN hyperbolic grid generator and the HGUI graphical user interface , 1993 .

[8] T. Coakley,et al. Turbulence Modeling Validation, Testing, and Development , 1997 .