Some Experiments on Hypersonic Separated Flows
- 1 October 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in ARS Journal
- Vol. 32 (10), 1564-1572
- https://doi.org/10.2514/8.6334
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- An Investigation of Separated Flows- Part I I : Flow in the Cavity and Heat TransferJournal of the Aerospace Sciences, 1961
- An Investigation of Separated Flows - Part I: The Pressure FieldJournal of the Aerospace Sciences, 1961
- Heat Transfer in Separated FlowsJournal of the Aerospace Sciences, 1959
- IV. Experiments on supersonic flow past bodies of revolution with annular gaps of rectangular sectionThe London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science, 1955
- Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause SeparationJournal of the Aeronautical Sciences, 1953
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953
- A Mixing Theory for the Interaction Between Dissipative Flows and Nearly Isentropic StreamsJournal of the Aeronautical Sciences, 1952
- LXVIII. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air streamThe London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science, 1952
- III. The interaction between an oblique shock-wave and a turbulent boundary-layerThe London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science, 1951