Turbulent boundary layer solution for two-dimensional compressible flow using mixing length and K-[epsilon] turbulence models
By: by M. Khalid.
Contributors: National Research Council of Canada.; Institute for Aerospace Research (Canada)
Series: National Research Council Canada -- 32135; Aeronautical Note / Institute for Aerospace Research -- AN69
Publisher: National Research Council Canada
Published: 1990
Place of publication: Ottawa
Language: eng