A method of solving the three-dimensional laminar boundary-layer equations with application to a lifting re-entry body.
- 1 June 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (6), 1075-1084
- https://doi.org/10.2514/3.4676
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Displacement thickness for boundary layers with surface mass transfer.AIAA Journal, 1966
- The numerical solution of boundary‐layer problemsAIChE Journal, 1965
- The Boundary Layer on a Townend SurfaceAeronautical Quarterly, 1965
- Chemical and vibrational relaxation of an inviscid hypersonic flowAIAA Journal, 1964
- SECOND-ORDER COMPRESSIBLE BOUNDARY LAYER THEORY WITH APPLICATION TO BLUNT BODIES IN HYPERSONIC FLOWPublished by Elsevier ,1962
- Nonsimilar Solutions of the Compressible-Laminar Boundary-Layer Equations With Applications to the Upstream-Transpiration Cooling ProblemJournal of the Aerospace Sciences, 1961
- Laminar Heat Transfer on Three-Dimensional Blunt Nosed Bodies in Hypersonic FlowARS Journal, 1959
- On displacement thicknessJournal of Fluid Mechanics, 1958
- Three-Dimensional Boundary Layer TheoryPublished by Elsevier ,1956