The flow about a slender cone at hypersonic speeds in the weak interaction regime
- 21 June 1971
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- The flow about a slender cone at hypersonic speeds in the weak interaction regimePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Flow field measurements using a total temperature probe at hypersonicspeedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Viscous Interaction Theory for Slender Axisymmetric Bodies in Hypersonic FlowAIAA Journal, 1968
- Hypersonic viscous interaction on slender conesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- Hypersonic viscous interaction theory for slender axisymmetric bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968
- EFFECTS OF NOSE BLUNTNESS ON THE BOUNDARY LAYER CHARACTERISTICS OF CONICAL BODIES AT HYPERSONIC SPEEDSPublished by Defense Technical Information Center (DTIC) ,1966
- Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodiesJournal of Fluid Mechanics, 1964
- BOUNDARY CONDITIONS AT THE OUTER EDGE OF THE BOUNDARY LAYER ON BLUNTED CONICAL BODIESAIAA Journal, 1963
- Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight SpeedsJournal of Jet Propulsion, 1956