**Author details**

Unver Kaynak1 \*, Onur Bas2 , Samet Caka Cakmakcioglu3 and Ismail Hakki Tuncer4


\*Address all correspondence to: unkaynak@gmail.com

© 2019 The Author(s). Licensee IntechOpen. This chapter is distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/ by/3.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

**119**

*Transition Modeling for Low to High Speed Boundary Layer Flows with CFD Applications*

correlation based transition model using local variables: Part I—Model Formulation. In: ASME Turbo Expo 2004, Power for Land, Sea, and Air, Vienna, Austria; 14-17 June 2004; Paper

[11] Langtry RB, Menter FR. Transition modeling for general cfd applications in aeronautics. In: 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA; 10-13 January 2005; Paper No.

[12] Lodefier K, Merci B, De Langhe C, Dick E. Transition Modeling with the SST Turbulence Model and Intermittency Transport Equation. In: ASME Turbo Expo 2003, Power for Land, Sea, and Air, Atlanta, GA, USA; 16-19 June 2003; Paper No.

[13] Walters DK, Leylek JH. A new model for boundary-layer transition using a single point RANS approach. ASME Journal of Turbomachinery.

[14] Walters DK, Cokljat D. A threeequation Eddy-viscosity model for Reynolds-averaged Navier-stokes simulations of transitional flow. ASME Journal of Fluids Engineering.

No. GT2004-53452

2005-522

GT2003-38282

2004;**126**(1):193-202

2008;**130**(12):121401

[15] Fu S, Wang L. A transport intermittency model for supersonic/ hypersonic boundary layer transition.

In: 5th European Congress on Computational Methods in Applied Sciences and Engineering (ECCOMAS),

Venice, Italy; 30 June-5 July 2008

[16] Seyfert C, Krumbein A. Correlationbased transition transport modeling for three-dimensional aerodynamic configurations. In: 50th AIAA

Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, Tennessee,

*DOI: http://dx.doi.org/10.5772/intechopen.83520*

[1] Menter FR, Langtry RB, Völker S. Transition modeling for general purpose CFD codes. Flow, Turbulence and Combustion. 2002;**77**:277-303

[2] Smith AMO, Gamberoni N. Pressure Gradient and Stability Theory. Report No. ES 26388. Long Beach, CA: Douglas

[3] Van Ingen JL. A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region. Report VTH-74. The Netherlands: Delft University of Technology, Department of Aerospace Engineering; 1956

[4] Drela M, Giles MB. Viscous-inviscid analysis of transonic and low Reynolds

number airfoils. AIAA Journal.

[5] Jones WP, Launder BE. The calculation of low Reynolds number phenomena with a two-equation model of turbulence. International Journal of Heat and Mass Transfer.

[6] Dhawan S, Narasimha R. Some properties of boundary layer during transition from laminar to turbulent flow motion. Journal of Fluid Mechanics. 1958;**3**(04):418-436

[7] Steelant J, Dick E. Modeling of laminar-turbulent transition for high freestream turbulence. ASME Journal of Fluids Engineering. 2000;**123**(1):22-30

[8] Cho JR, Chung MK. A k—ε—γ equation turbulence model. Journal of Fluid Mechanics. 1992;**237**:301-322

[9] Suzen YB, Huang PG. Modeling

[10] Menter FR, Langtry RB, Likki SR, Suzen YB, Huang PG, Völker S. A

of flow transition using an intermittency transport equation. ASME Journal of Fluids Engineering.

2000;**122**(2):273-284

1987;**25**(10):1347-1355

1973;**15**(2):301-314

Aircraft Company; 1956

**References**

*Transition Modeling for Low to High Speed Boundary Layer Flows with CFD Applications DOI: http://dx.doi.org/10.5772/intechopen.83520*
