Turbulence measurements in a compressible boundary layer subjected to a shock-wave-induced adverse pressure gradient
- 10 January 1973
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Turbulence measurements in a compressible boundary layer subjected to a shock-wave-induced adverse pressure gradientPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20AIAA Journal, 1971
- Fluctuation Measurements in a Supersonic Turbulent Boundary LayerPhysics of Fluids, 1959
- Turbulence in Supersonic FlowJournal of the Aeronautical Sciences, 1953
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950