Turbulence modeling ; Turbulence compressibility corrections ; Three-dimensional Navier-Stokes method with two-equation turbulence models for efficient numerical simulation of hypersonic flows ; Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3
By: Jorge E. Bardina, Thomas J. Coakley, C. C. Horstman, Joseph G. Marvin, John R. Viegas, P. G. Huang and Marvin I. Kussoy.
Contributors: Coakley, Thomas J.; Horstman, C. C.; Huang, P. G.; Kussoy, Marvin I.; Marvin, Joseph G.; Viegas, John R.; MCAT Institute
Series: MCAT Institute progress report -- 95-04
Publisher: MCAT Institute
Published: 1995
Place of publication: San Jose, Calif
Subjects: Turbulence models
Notes: Includes 3 papers as appendices: Turbulence compressibility corrections / T.J. Coakley [et al.], NASA TM 108827; Three-dimensional Navier-Stokes method with two-equation turbulence models for efficient numerical simulation of hypersonic flows / J.E. Bardina, AIAA 94-2950; and Three-dimensional Navier-Stokes simulations with two-equation turbulence models of intersecting shock-waves/turbulent boundary layer at Mach 8.3 / J.E. Bardina, T.J. Coakley, AIAA 94-1905.

Includes bibliographical references.