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ABLATION COOLING OF MISSILES AND SATELLITES
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English
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ECKERT, E., "ABLATION COOLING OF MISSILES AND SATELLITES," SAE Technical Paper 600170, 1960, https://doi.org/10.4271/600170.Also In
References
- Hayday A. A. Mass Transfer Cooling in a Steady Laminar Boundary Layer Near the Stagnation Point 156 169 Heat Transfer and Fluid Mechanics Institute Stanford Stanford University Press 1959
- Eckert E. R. G. Schneider P. J. Hayday A. A. Larson R. M. Mass-transfer Cooling of a Laminar Boundary Layer by Injection of a Light-Weight Foreign Gas Jet Propulsion 28 34 39 1959
- Leadon B. M. Scott C. J. Transpiration Cooling Experiments in a Turbulent Boundary Layer at M = 3 J. Aeronaut. Sci. 23 798 99 1956
- Rubesin M. W. Pappas C. C. An Analysis of the Turbulent Boundary-Layer Characteristics on a Flat Plate with Distributed Light-gas Injection 1958
- Lees L. Convective Heat Transfer with Mass Addition and Chemical Reactions, Combustion and Propulsion Third Agard Colloquium New York Pergamon Press 451 1958
- Sutton George W. Ablation of Reinforced Plastics in Supersonic Flow Journ. Aero/Space Sci. 27 377 1960
- Gross J. F. Hartnett J. P. Gazley C. Masson D. J. Effect of Molecular Weight on Mass-Transfer Cooling in a Laminar Boundary-Layer on a Flat Plate. To be published in Journ. Aero/Space Sciences
- Scott C. J. The Application of Constant Property Solutions to Mass Transfer Cooling, Eng. Memo 76 1958 Minneapolis University of Minnesota, Rose-mount Aeronautical Laboratories
- Hartnett J. P. Masson D. J. Gross J. F. Gazley C. Mass Transfer Cooling in a Turbulent Boundary Layer. To be published in Journ. Aero/Space Sciences