Heat Transfer in a Transitional and Turbulent Boundary Layer at Supersonic Speeds
- 1 September 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (9), 646-647
- https://doi.org/10.2514/8.2775
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- On Boundary-Layer Temperature Recovery FactorsJournal of the Aeronautical Sciences, 1952
- A Solution of the Laminar Boundary-Layer Equations for a Compressible Fluid with Variable Properties, Including DissociationJournal of the Aeronautical Sciences, 1952
- Recent Investigation of Temperature Recovery and Heat Transmission on Cones and Cylinders in Axial Flow in the N.O.L. Aeroballistics Wind TunnelJournal of the Aeronautical Sciences, 1952