Numerical Solution of Supersonic Laminar Flow Over an Inclined Body of Revolution
- 1 August 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (8) , 921-928
- https://doi.org/10.2514/3.50835
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- On implicit finite-difference simulations of three-dimensional flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Concentrated vortex on the nose of an inclined body of revolutionAIAA Journal, 1976
- Three-dimensional supersonic flow of a viscous or inviscid gasJournal of Computational Physics, 1975
- Experiments on Supersonic Boundary-Layer Separation in Three DimensionsJournal of Applied Mechanics, 1975
- A numerical method for solving the Navier-Stokes equations with application to shock-boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layerJournal of Fluid Mechanics, 1973
- Boundary-Layer Separation on Slender Cones at Angle of AttackAIAA Journal, 1972
- Analytic Difficulties in Predicting Dynamic Effects of Separated FlowJournal of Spacecraft and Rockets, 1971
- Numerical solution of the hypersonic viscous shock-layer equationsAIAA Journal, 1970
- Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactionsAIAA Journal, 1964