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Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code

Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction using the DLR TAU Code

썸네일 EDISON_Aero 애게서 업로드 하였습니다. 18. 10. 1 오전 10:48
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Krumbein A., Krimmelbein N. (2007) Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction Using the DLR TAU Code. In: Tropea C., Jakirlic S., Heinemann HJ., Henke R., Hönlinger H. (eds) New Results in Numerical and Experimental Fluid Mechanics VI. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 96. Springer, Berlin, Heidelberg DOI https://doi.org/10.1007/978-3-540-74460-3_26
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Krumbein A., Krimmelbein N. (2007) Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction Using the DLR TAU Code. In: Tropea C., Jakirlic S., Heinemann HJ., Henke R., Hönlinger H. (eds) New Results in Numerical and Experimental Fluid Mechanics VI. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 96. Springer, Berlin, Heidelberg DOI https://doi.org/10.1007/978-3-540-74460-3_26
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