Advanced k-epsilon modeling of heat transfer

By: Nasa, National Aeronautics and Space Adm

This report describes two approaches to low Reynolds-number k-epsilon turbulence modeling which formulate the eddy viscosity on the wall-normal component of turbulence and a length scale. The wall-normal component of turbulence is computed via integration of the energy spectrum based on the local dissipation rate and is bounded by the isotropic condition. The models account for the anisotropy of the dissipation and the reduced mixing length due to the high strain rates present in the near-wall region. The turbulent kinetic energy and its dissipation rate were computed from the k and epsilon transport equations of Durbin. The models were tested for a wide range of turbulent flows and proved to be superior to other k-epsilon models, especially for nonequilibrium anisotropic flows. For the prediction of airfoil heat transfer, the models included a set of empirical correlations for predicting laminar-turbulent transition and laminar heat transfer augmentation due to the presence of freestream turbulence. The predictions of surface heat transfer were generally satisfactory. Kwon, Okey and Ames, Forrest E. AERODYNAMIC HEAT TRANSFER; BOUNDARY LAYER FLOW; COMPUTATIONAL FLUID DYNAMICS; EDDY VISCOSITY; K-EPSILON TURBULENCE MODEL; LOW REYNOLDS NUMBER; TURBULENCE; TURBULENT FLOW; ANISOTROPY; KINETIC ENERGY; MIXING LENGTH FLOW THEORY; NONEQUILIBRIUM FLOW; TURBINE BLADES; WALL FLOW...

• Format: Paperback
• Language: English
• ISBN: 1731341407
• ISBN13: 9781731341402
• Release Date: January 1
• Publisher: Independently Published
• Length: 158 Pages
• Weight: 0.84 lbs.
• Dimensions: 0.3" x 8.5" x 11.0"