Aerodynamic noise and boundary-layer transition measurements in supersonic test facilities.
- 1 November 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (11) , 1531-1532
- https://doi.org/10.2514/3.6654
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Hypersonic boundary-layer transition in the presence of wind-tunnel noise.AIAA Journal, 1971
- SYNOPTIC: 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
- The Mach wave field radiated by supersonic turbulent shear flowsJournal of Fluid Mechanics, 1965
- Aerodynamic Noise in Supersonic Wind TunnelsJournal of the Aerospace Sciences, 1961