Supersonic laminar boundary layer along a two- dimensional adiabaticcurved ramp.
- 1 February 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (2) , 298-304
- https://doi.org/10.2514/3.5089
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Theory of laminar viscous-inviscid interactions in supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling.AIAA Journal, 1968
- A second-order weak interaction expansion for moderately hypersonic flow past a flat plate.AIAA Journal, 1967
- Laminar boundary-layer separation and near-wake flow for a smooth blunt body at supersonic and hypersonic speeds.AIAA Journal, 1967
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964