Calculations are presented for the forces on a thin supersonic wing underneath which the air is heated. The analysis is limited principally to linearized theory but nonlinear effects are considered. It is shown that significant advantages to external heating would exist if the heat were added well below and ahead of the wing.
Two-Dimensional, Supersonic, Linearized Flow with Heat Addition
1959-02-01
Sonstige
Keine Angabe
Englisch
Vorticity Distribution in Linearized Supersonic Flow
AIAA | 2018
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Engineering Index Backfile | 1947
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