Experimental investigation of far wakes behind two-dimensional slender bodies at M sub infinity equals 6
- 24 June 1968
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Experimental investigation of laminar near wakes behind 20 deg wedges at M infinity equals 6Published by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Measurements of the turbulent near wake of a cone at Mach 6.AIAA Journal, 1966
- Hypersonic wakes and trailsAIAA Journal, 1964
- Viscous interaction effects on a static pressure probe at m equals 6AIAA Journal, 1963
- The mechanism of transition in the wake of a thin flat plate placed parallel to a uniform flowJournal of Fluid Mechanics, 1961
- An Experimental Investigation of Base Flows at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1961