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Mandatory calculations the LEISA high lift airfoil S.Reuß

Mandatory calculations the LEISA high lift airfoil S.Reuß. Settings for mandatory RANS calculations. Use new mandatory grid that can be found on the website Transition locations: Angles of attack of 5°, 6° and 7° Spalart-Allmaras model Menter SST-k ω model

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Mandatory calculations the LEISA high lift airfoil S.Reuß

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  1. Mandatory calculations the LEISA high lift airfoilS.Reuß

  2. Settings for mandatory RANS calculations • Use new mandatory grid that can be found on the website • Transition locations: • Angles of attack of 5°, 6° and 7° • Spalart-Allmaras model • Menter SST-kω model • If you use another RANS model in your DES, please also compute the three angles with this model • ATTENTION: IT TAKES A LARGE NUMBER OF ITERATIONS TILL THE CALCULATIONS CONVERGE!

  3. Pressure distribution SA / SST model SA model SST model

  4. Skin friction SA / SST model SA model SST model

  5. Seperation above the flap SA / SST SA model α=6° SST model α=5°

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