A method for direct shear measurement of large scale roughened surfaces in short duration hypersonic facilities
This paper focuses on the development process of a floating element shear stress measurement device for testing in a short duration hypersonic wind tunnel. First experiments have been carried out in the Oxford High Density Tunnel at a nominal Mach number of 5 with unit Reynolds numbers 44 - 62×106 m...
| Main Authors: | , , , |
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| Format: | Conference item |
| Language: | English |
| Published: |
American Institute of Aeronautics and Astronautics (AIAA)
2023
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