Mean and fluctuating flow measurements in the hypersonic boundary layer over a cooled wall
- 18 March 1974
- journal article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 63 (01) , 121
- https://doi.org/10.1017/s0022112074001042
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Development of a Hot-Wire Anemometer for Hypersonic Turbulent FlowsReview of Scientific Instruments, 1972
- Turbulent front structure of an axisymmetric compressible wakeJournal of Fluid Mechanics, 1968
- Turbulence Measurements in an Axisymmetric Compressible WakePhysics of Fluids, 1968
- Some Statistical Properties of the Pressure Field Radiated by a Turbulent Boundary LayerPhysics of Fluids, 1964
- The fluctuating pressure field in a supersonic turbulent boundary layerJournal of Fluid Mechanics, 1963
- Fluctuation Measurements in a Supersonic Turbulent Boundary LayerPhysics of Fluids, 1959
- The law of the wake in the turbulent boundary layerJournal of Fluid Mechanics, 1956
- Turbulence in Supersonic FlowJournal of the Aeronautical Sciences, 1953
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950