A comparison of disturbance levels measured in hypersonic tunnels using a hot-wire anemometer and a pitot pressure probe
- 16 August 1972
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Surface pressure fluctuations near an axisymmetric stagnation pointPublished by National Institute of Standards and Technology (NIST) ,1971
- Effects of freestream disturbances on boundary-layer transition.AIAA Journal, 1968
- Effects of freestream turbulence on boundary- layer transition.AIAA Journal, 1967
- Hot Wire Measurements in Low Reynolds Number Hypersonic FlowsARS Journal, 1961