Active cooling heat protection.
- 1 June 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 6 (6), 661-666
- https://doi.org/10.2514/3.29637
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- Transpiration cooling in a laminar boundary layer with solid wall upstream effects.AIAA Journal, 1968
- Turbulent heat-transfer and skin-friction measurements on a porous cone with air injection at high Mach numbers.AIAA Journal, 1966
- Film cooling with air and helium injection through a rearward-facingslot into a supersonic air flow.AIAA Journal, 1966
- A note on the use of a boundary-layer model for correlating film-cooling dataInternational Journal of Heat and Mass Transfer, 1965
- Transpiration cooling of a turbulent boundary layer in an axisymmetric nozzleAIAA Journal, 1964
- Velocity Distributions, Temperature Distributions, Effectiveness and Heat Transfer for Air Injected Through a Tangential Slot Into a Turbulent Boundary LayerJournal of Heat Transfer, 1961