Compressible turbulent boundary layer with pressure gradient and heat transfer.
- 1 January 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (1) , 19-25
- https://doi.org/10.2514/3.3378
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- The Turbulent Boundary Layer in a Compressible FluidPhysics of Fluids, 1964
- Study of the incompressible turbulent boundary layer with pressure gradientAIAA Journal, 1964
- Laminar, Transitional and Turbulent Heat Transfer to a Cone-Cylinder-Flare Body at Mach 8.0Journal of the Aerospace Sciences, 1962
- The Application of the Reference-Enthalpy Method to Friction FormulasJournal of the Aerospace Sciences, 1962
- The Effect of Adverse Pressure Gradients on the Characteristics of Turbulent Boundary Layers in Supersonic StreamsJournal of the Aerospace Sciences, 1962
- An Investigation of Laminar, Transitional, and Turbulent Heat Transfer on Blunt-Nosed Bodies in Hypersonic FlowJournal of the Aerospace Sciences, 1960
- Transformation of the Compressible Turbulent Boundary LayerJournal of the Aerospace Sciences, 1958
- The Turbulent Boundary LayerPublished by Elsevier ,1956