It is shown that aerodynamic heating is reduced substantially by injecting small quantity of coolant into boundary layer; laminar boundary layer may be maintained at high supersonic speeds and high Reynolds numbers even with fluid injections.
Analysis of supersonic aerodynamic heating with continuous fluid injection
Nat Advisory Committee Aeronautics -- Tech Note
1949
31 pages
Charts
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English
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Analysis of supersonic aerodynamic heating with continuous fluid injection
Engineering Index Backfile | 1950
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