Hypersonic boundary-layer transition data for a cold-wall slender cone
- 1 April 1965
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (4) , 758-760
- https://doi.org/10.2514/3.2969
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Laminar, Transitional and Turbulent Heat Transfer to a Cone-Cylinder-Flare Body at Mach 8.0Journal of the Aerospace Sciences, 1962
- Boundary-Layer Transition on Blunt Bodies with Highly Cooled Boundary LayersJournal of the Aerospace Sciences, 1960
- On Laminar Boundary Layers With Heat TransferJournal of Jet Propulsion, 1956