Article

Heat and Mass Transfer and Physical Gasdynamics
2016. V. 54. № 3. P. 377–382
Lushchik V.G., Makarova M.S.
Numerical investigation of the effect of the Prandtl number on the temperature recovery and the Reynolds analogy factors in the boundary layer on a plate
Annotation
We performed a numerical study of the boundary layer on a wall in a supersonic gas flow using a differential turbulence model. The dependences of the recovery factor and the Reynolds analogy factor on the main flow parameters, such as the Reynolds, Mach, and Prandtl numbers, are obtained for a series of the temperature factor values. The results of calculations are approximated by the dependences of the recovery factor and the Reynolds analogy factor on the Prandtl number.
Article reference:
Lushchik V.G., Makarova M.S. Numerical investigation of the effect of the Prandtl number on the temperature recovery and the Reynolds analogy factors in the boundary layer on a plate, High Temp., 2016. V. 54. № 3. P. 377