An experimental investigation of boundary layer and heat transfer inthe region of separated flow downstream of normal injection slots
Author:
Affiliation:
1. LTV Aerospace Corp., Vought Systems Div., Dallas, Tex.
2. Texas, University, Arlington, Tex.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1974-678
Reference13 articles.
1. Velocity Distributions, Temperature Distributions, Effectiveness and Heat Transfer for Air Injected Through a Tangential Slot Into a Turbulent Boundary Layer
2. Film Cooling of an Adiabatic Flat Plate in Zero Pressure Gradient in the Presence of a Hot Mainstream and Cold Tangential Secondary Injection
3. Film cooling with air and helium injection through a rearward-facingslot into a supersonic air flow.
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. An Experimental Investigation of Film Cooling Heat Transfer Coefficients Using the Mass/Heat Analogy;Journal of Heat Transfer;1995-11-01
2. Full-coverage film cooling. Part 1. Three-dimensional measurements of turbulence structure;Journal of Fluid Mechanics;1980-11-13
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