Experimental investigation of laminar near wakes behind 20 deg wedges at M infinity equals 6
- 22 January 1968
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Measurements of the turbulent near wake of a cone at Mach 6.AIAA Journal, 1966
- Near wake of a blunt body at hypersonic speedsAIAA Journal, 1965
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949