Three-Dimensional Supersonic Viscous Flow over a Cone at Incidence
- 1 November 1982
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (11) , 1500-1507
- https://doi.org/10.2514/3.51213
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A two-layer model for coupled three-dimensional viscous and inviscid flow calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Non-Navier Stokes viscous flow computationsComputers & Fluids, 1980
- An implicit method for three dimensional viscous flow with application to cones at angle of attackComputers & Fluids, 1975
- Viscous flow over a cone at moderate incidence. Part 2. Supersonic boundary layerJournal of Fluid Mechanics, 1973
- Viscous flow over a cone at moderate incidence—IComputers & Fluids, 1973
- Experimental and theoretical study of supersonic viscous flow over ayawed circular cone.AIAA Journal, 1972