Experimental investigation of the mean flow of the laminar supersonic cone wake
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (3) , 479-484
- https://doi.org/10.2514/3.6206
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
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- Experimental Investigation of Laminar Near Wakes Behind 20 Wedges M=6AIAA Journal, 1968
- The far wake behind cylinders at hypersonic speeds. I.AIAA Journal, 1967
- Measurements of the turbulent near wake of a cone at Mach 6.AIAA Journal, 1966
- An experimental investigation of the near wake of a slender cone at M infinity equal 8 and 12.AIAA Journal, 1966
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- Viscous interaction effects on a static pressure probe at m equals 6AIAA Journal, 1963
- Magnetic Suspension and Balance System for Wind Tunnel ApplicationJournal of the Royal Aeronautical Society, 1963
- SUPPORT INTERFERENCE EFFECTS ON THE SUPERSONIC WAKEAIAA Journal, 1963