Preliminary results from an experimental investigation of nozzle wall boundary layer at Mach numbers ranging from 27 to 47
- 16 June 1969
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Some observations on reduction of turbulent boundary-layer heat transfer in nozzles.AIAA Journal, 1966
- The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transferJournal of Fluid Mechanics, 1964
- PRESSURES IN THE STAGNATION REGIONS OF BLUNT BODIES IN THE VISCOUS-LAYER TO MERGED-LAYER REGIMES OF RAREFIED FLOWPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963
- Turbulent Boundary Layer Measurements at Mach Numbers from 8 to 10Physics of Fluids, 1959