Tangential slot injection in supersonic flow.
- 1 December 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (12), 2149-2154
- https://doi.org/10.2514/3.4400
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Film cooling with air and helium injection through a rearward-facingslot into a supersonic air flow.AIAA Journal, 1966
- An Analytical and Experimental Study of the Plane, Incompressible, Turbulent Free-Shear Layer With Arbitrary Velocity Ratio and Pressure GradientJournal of Basic Engineering, 1965
- Initial Boundary Layer Effects on Laminar Flows With Wall Slot InjectionJournal of Heat Transfer, 1965
- APPROXIMATE ANALYSIS OF THE SLOT INJECTION OF A GAS IN LAMINAR FLOWAIAA Journal, 1963
- Velocity Distributions, Temperature Distributions, Effectiveness and Heat Transfer for Air Injected Through a Tangential Slot Into a Turbulent Boundary LayerJournal of Heat Transfer, 1961
- The two-dimensional turbulent wall-jetJournal of Fluid Mechanics, 1961
- Heat Transfer and Effectiveness for a Turbulent Boundary Layer With Tangential Fluid InjectionJournal of Heat Transfer, 1960
- The Turbulent Boundary LayerPublished by Elsevier ,1956