A Computational Approach to Simulating the Effects of Realistic Surface Roughness on Boundary Layer Transition.
暂无分享,去创建一个
[1] Thomas H. Pulliam,et al. Recent enhancements to OVERFLOW , 1997 .
[2] M. V. Morkovin,et al. Experiments on transition enhancement by distributed roughness , 1986 .
[3] W. A. Timmer,et al. Roughness Sensitivity Considerations for Thick Rotor Blade Airfoils , 2003 .
[4] J. Nikuradse. Laws of Flow in Rough Pipes , 1950 .
[5] C. P. van Dam,et al. Transition prediction for a two‐dimensional reynolds‐averaged navier–stokes method applied to wind turbine airfoils , 2001 .
[6] S. Wittig,et al. Extended Models for Transitional Rough Wall Boundary Layers With Heat Transfer—Part I: Model Formulations , 2009 .
[7] Hugh L. Dryden. Combined effects of turbulence and roughness on transition , 1958 .
[8] Michael Fort Kerho. Effect of large distributed roughness near an airfoil leading edge on boundary layer development and transition , 1995 .
[9] Paul A. Durbin,et al. Rough Wall Modification of Two-Layer k−ε , 2001 .
[10] M. Kerho,et al. Effect of large distributed leading-edge roughness on boundary layer development and transition , 1995 .
[11] Michael B. Bragg,et al. Airfoil boundary-layer development and transition with large leading-edge roughness , 1997 .
[12] B. J. Abu-Ghannam,et al. Natural Transition of Boundary Layers—The Effects of Turbulence, Pressure Gradient, and Flow History , 1980 .
[13] E. R. V. Driest,et al. BOUNDARY LAYER TRANSITION--FREE-STREAM TURBULENCE AND PRESSURE GRADIENT EFFECTS, , 1963 .
[14] A D Young,et al. Aircraft Excrescence Drag , 1981 .
[15] M. S. Acarlar,et al. A study of hairpin vortices in a laminar boundary layer. Part 1. Hairpin vortices generated by a hemisphere protuberance , 1987, Journal of Fluid Mechanics.
[16] P S Klebanoff,et al. MECHANISM BY WHICH A TWO-DIMENSIONAL ROUGHNESS ELEMENT INDUCES BOUNDARY-LAYER TRANSITION: ROUGHNESS INDUCED TRANSITION , 1972 .
[17] Florian R. Menter,et al. Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes , 2009 .
[18] Robert S. Ehrmann,et al. Realistic Leading-Edge Roughness Effects on Airfoil Performance. , 2013 .
[19] J. V. Ingen. The eN method for transition prediction: Historical review of work at TU Delft , 2008 .
[20] Charles L. Merkle,et al. An Analytical Study of the Effects of Surface Roughness on Boundary-Layer Transition , 1974 .
[21] Robin Blair Langtry,et al. A correlation-based transition model using local variables for unstructured parallelized CFD codes , 2011 .
[22] Christopher L. Rumsey,et al. Effective Inflow Conditions for Turbulence Models in Aerodynamic Calculations , 2007 .
[23] D. Wilcox. Turbulence modeling for CFD , 1993 .
[24] E. Mayda. Boundary-layer transition prediction for Reynolds -averaged Navier -Stokes methods , 2007 .
[25] Esteban Ferrer,et al. CFD predictions of transition and distributed roughness over a wind turbine airfoil , 2009 .
[26] Siva Nadarajah,et al. Laminar‐turbulent flow simulation for wind turbine profiles using the γ–Re˜θt transition model , 2014 .
[27] R. F. Warming,et al. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations , 1977 .
[28] T. Esch,et al. TRANSITION MODELLING BASED ON LOCAL VARIABLES , 2002 .
[29] Seppo Laine,et al. Extension of the k-omega-SST turbulence model for flows over rough surfaces , 1997 .