Structure of the boundary layer at the leading edge of a flat plate in hypersonic slip flow
- 1 September 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (9) , 1655-1657
- https://doi.org/10.2514/3.2641
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The effect of compositional variables upon oscillatory combustion of solid rocket propellantsCombustion and Flame, 1964
- CRITERION FOR SLIP NEAR THE LEADING EDGE OF A FLAT PLATE IN HYPERSONIC FLOWAIAA Journal, 1963
- The Free Molecule Probe and Its Use for the Study of Leading Edge FlowsPhysics of Fluids, 1958