作者: F. R. Menter , M. Kuntz
DOI: 10.1007/978-3-540-44419-0_30
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摘要: Turbulence model development for aerodynamic applications has many years concentrated on improving the capabilities of CFD methods separation prediction. Validation studies turbulence models in ‘80th have clearly shown that most were not capable predicting turbulent boundary layers under adverse pressure gradient conditions. Based observation, new developed to specifically meet this challenge, resulting a series capturing layer good agreement with experimental data (Johnson and King 1984, Menter 1993, Spalart Allmaras 1994).