Calculations of the compressible turbulent boundary layer with pressure gradient and heat transfer in internal flowswith particular reference to supersonic nozzles
By: by E.R. Bergstrom and S. Raghunathan.
Contributors: Raghunathan, S.; Loughborough University of Technology. Department of Transport Technology.
Series: TT 7104
Publisher: Loughborough University of Technology, Department of Transport Technology
Published: 1971
Place of publication: Loughborough
Language: eng