Hot-wire accuracy in supersonic turbulence from comparisons with laser-induced fluorescence
- 1 March 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 26 (3) , 316-322
- https://doi.org/10.2514/3.9891
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Measurements of temperature, density, pressure, and their fluctuations in supersonic turbulence using laser-induced fluorescenceExperiments in Fluids, 1987
- Measurements of fluctuating temperatures in a supersonic turbulent flow using laser-induced fluorescenceAIAA Journal, 1985
- The Structure of Turbulence in a Supersonic Shock-Wave/Boundary-Layer InteractionAIAA Journal, 1984
- Preliminary measurements of velocity, density and total temperature fluctuations in compressible subsonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Buckling analysis of geometrically imperfect stiffened cylinders under axial compressionAIAA Journal, 1977
- Turbulence stress measurements in a nonadiabatic hypersonic boundarylayerAIAA Journal, 1975
- Laser Velocimeter and Hot-wire Anemometer Comparison in a Supersonic Boundary LayerAIAA Journal, 1975
- Fluctuation Measurements in a Supersonic Turbulent Boundary LayerPhysics of Fluids, 1959
- Turbulence in Supersonic FlowJournal of the Aeronautical Sciences, 1953
- The Hot-Wire Anemometer in Supersonic FlowJournal of the Aeronautical Sciences, 1950