Nozzle Wall Boundary-Layer Transition and Freestream Disturbances at Mach 5
- 1 March 1975
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 13 (3) , 307-314
- https://doi.org/10.2514/3.49696
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Development of a High Reynolds Number Quiet Tunnel for Transition ResearchAIAA Journal, 1975
- Influence of measured freestream disturbances on hypersonic boundary-layer transitionAIAA Journal, 1970
- Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels.AIAA Journal, 1969
- Effects of acoustic feedback on the spread and decay of supersonic jets.AIAA Journal, 1968
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961
- On Supersonic Wind Tunnels With Low Free-Stream DisturbancesJournal of Applied Mechanics, 1959