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...
| Päätekijät: | , , , |
|---|---|
| Aineistotyyppi: | Conference item |
| Kieli: | English |
| Julkaistu: |
American Institute of Aeronautics and Astronautics (AIAA)
2023
|