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- W2166470178 abstract "This paper describes the Computational Fluid Dynamics (CFD) efforts and lessons learned during the four-year Abrupt Wing Stall national research program. The paper details the complex nature of the transonic flows encountered by modern U.S. fighter and attack aircraft during transonic maneuvering conditions. Topics include grid resolution, computational memory and CPU requirements, turbulence modeling, steady and unsteady calculations, and Reynolds-Averaged-Navier-Stokes solutions compared with Detached Eddy Simulations for this highly complex, viscously-dominated, shock-induced, massively-separated class of flow. Examples include results obtained for F/A-18C, AV-8B, pre-production F/A-18E, and F-16N aircraft undergoing transonic maneuvering conditions. Various flap settings have been modeled and the CFD results compared with extensive wind tunnel data. The comparisons illustrate the results obtained from both structured and unstructured CFD codes. The utility and accuracy of the various computational solvers is evaluated by qualitative comparisons of surface oil flow and pressure sensitive paint results obtained in wind tunnels for some of the models as well as by detailed quantitative pressure coefficient data where experimental results exist. Static lift coefficients are compared between CFD codes as well as the experimental data for each of the aircraft considered in this study." @default.
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- W2166470178 date "2003-01-06" @default.
- W2166470178 modified "2023-10-14" @default.
- W2166470178 title "UNDERSTANDING ABRUPT WING STALL WITH CFD" @default.
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- W2166470178 doi "https://doi.org/10.2514/6.2003-592" @default.
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