A comparison of the predictive capabilities of several turbulence models using upwind and central-difference computer codes

Author:

RUMSEY CHRISTOPHER1,VATSA VEER1

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Reference27 articles.

1. tions on theONERAM6Wing at Transonic Mach Numbers," ACARD AR-138,p. B1, 1979.

2. Application of Transonic Wing and Far-Field Test Data for Three-Dimensional Computational Method Evaluation, Volume 11 -Appendix B, Experimental Data," AFOSR-TR-804422,1980.

3. Multigrid Code for 3-D Navier-Stokes Equations and its Application to a Grid-Refinement Study," Computers & Fluids,vol. 18, no. 4, pp.391403,

4. imation and Algebraic Model for Separated Turbulent Flow," AIM 78-257,1978.

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