Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20
- 1 May 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (5), 826-834
- https://doi.org/10.2514/3.6282
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Influence of measured freestream disturbances on hypersonic boundary-layer transitionAIAA Journal, 1970
- Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental dataAIAA Journal, 1970
- Boundary-layer transition on sharp cones at hypersonic Mach numbers.AIAA Journal, 1968
- The influence of hole dimensions on static pressure measurementsJournal of Fluid Mechanics, 1960
- Fluctuation Measurements in a Supersonic Turbulent Boundary LayerPhysics of Fluids, 1959
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950