Binary boundary layers on sharp cones in low-density supersonic and hypersonic flow.
- 1 April 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (4) , 699-706
- https://doi.org/10.2514/3.5189
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Solution to the binary diffusion laminar boundary-layer equations with second-order transverse curvature.AIAA Journal, 1967
- Viscous hypersonic flow over pointed cones at low Reynolds numbers.AIAA Journal, 1967
- Displacement thickness for boundary layers with surface mass transfer.AIAA Journal, 1966
- Transverse Curvature Effects in Axisymmetric Hypersonic Boundary LayersAIAA Journal, 1964
- Hypersonic viscous drag effects on blunt slender conesAIAA Journal, 1964
- Effect of mass injection on the drag of a slender cone in hypersonic flowAIAA Journal, 1964
- Axisymmetric Viscous Flow Past Very Slender Bodies of RevolutionJournal of the Aerospace Sciences, 1962
- SECOND-ORDER COMPRESSIBLE BOUNDARY LAYER THEORY WITH APPLICATION TO BLUNT BODIES IN HYPERSONIC FLOWPublished by Elsevier ,1962