Laminar Boundary-Layer Temperature Recovery Factor on a Cone at Nominal Mach Number Six
- 1 January 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (1) , 65-66
- https://doi.org/10.2514/8.2922
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Comments on Location of Detached Shock Waves Ahead of Plane BodiesJournal of the Aeronautical Sciences, 1953
- A Method for Location of Detached Shock Waves Ahead of Plane BodiesJournal of the Aeronautical Sciences, 1953
- On Boundary-Layer Temperature Recovery FactorsJournal 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