Johnson et al. (1982) have provided a detailed comparison between a thoroughly documented transonic flow with shock-induced separations and solutions of the flow using the Navier-Stokes equations. According to this comparison, there were several deficiencies in the computations. The present investigation takes into account new experimental data which have been obtained in a larger wind tunnel with the same test model for a wider range of freestream Mach numbers. The results of new Navier-Stokes computations using more compatible boundary conditions are shown, and the effects of the turbulence model choice on predicting Mach number trends are assessed.
Prediction of transonic separated flows
AIAA Journal ; 22
1984-07-01
Miscellaneous
No indication
English
Prediction of Transonic Separated Flows
AIAA | 1984
|Computation of separated transonic turbulent flows
AIAA | 1975
|Computation of Separated Transonic Turbulent Flows
AIAA | 1976
|