On the prediction of two-dimensional supersonic viscous interactionsnear walls
- 1 February 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (2) , 182-188
- https://doi.org/10.2514/3.7313
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Shock wave-boundary layer interactions in laminar transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- On the Numerical Solution of Two-Dimensional, Laminar Compressible Flows With Imbedded Shock WavesJournal of Basic Engineering, 1972
- 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
- An interaction model of a supersonic laminar boundary layer on sharpand rounded backward facing steps.AIAA Journal, 1968
- Interacting supersonic laminar wake calculations by a finite difference method.AIAA Journal, 1967
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964
- Boundary-Layer Displacement and Leading-Edge Bluntness Effects in High-Temperature Hypersonic FlowJournal of the Aerospace Sciences, 1961
- Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause SeparationJournal of the Aeronautical Sciences, 1953
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952