Hot-wire measurements in the hypersonic wakes of slender bodies
- 16 August 1963
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- An Experimental Investigation of Leading-Edge Shock-Wave - Boundary-Layer Interaction at Mach 5.8Journal of the Aeronautical Sciences, 1957