Experimental Investigation of Laminar Near Wakes Behind 20 Wedges M=6
- 1 November 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (11), 2077-2083
- https://doi.org/10.2514/3.55432
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Experimental investigation of far wakes behind two-dimensional slender bodies at M sub infinity equals 6Published by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Dynamics of gases containing evaporable liquid droplets under a normal shock.AIAA Journal, 1966
- Near wake of a blunt body at hypersonic speedsAIAA Journal, 1965
- Analysis of Normal Shock Waves in Particle Laden GasJournal of Basic Engineering, 1964
- Some Properties of Shock Relaxation in Gas Flows Carrying Small ParticlesPhysics of Fluids, 1964
- Viscous interaction effects on a static pressure probe at m equals 6AIAA Journal, 1963
- Hot Wire Measurements in Low Reynolds Number Hypersonic FlowsARS Journal, 1961
- Shock waves in a dusty gasJournal of Fluid Mechanics, 1958
- Acceleration of Dust Particles by Shock WavesJournal of Applied Physics, 1957
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949