SUPERSONIC AND HYPERSONIC TWO-DIMENSIONAL LAMINAR FLOW OVER A COMPRESSION CORNER
- 19 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- A Finite-Difference Method for Boundary Layers with Reverse FlowAIAA Journal, 1972
- THEORETICAL AND EXPERIMENTAL STUDIES OF THE SHOCK WAVE-BOUNDARY LAYER INTERACTION ON COMPRESSION SURFACES IN HYPERSONIC FLOWPublished by Defense Technical Information Center (DTIC) ,1970
- Upstream Influence in Viscous Interaction ProblemsPhysics of Fluids, 1968
- The interaction of a shock wave with a laminar boundary layer†International Journal of Non-Linear Mechanics, 1968
- Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling.AIAA Journal, 1968
- CALCULATION OF LAMINAR SEPARATION WITH FREE INTERACTION BY THE METHOD OF INTEGRAL RELATIONS. PART 1. TWO-DIMENSIONAL SUPERSONIC ADIABATIC FLOWPublished by Defense Technical Information Center (DTIC) ,1965
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964