Method developed consistent with assumptions of small perturbation theory, which provides means of determining downwash behind wing in supersonic flow for known load distribution; analysis based upon use of supersonic doublets distributed over plan form and wake of wing in manner determined from wing loading.
Calculation of downwash behind supersonic wings with application to triangular plan forms
Nat Advisory Committee Aeronautics -- Tech Note
1948
43 pages
Report
English
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Calculation of downwash behind supersonic wings with application to triangular plan forms
Engineering Index Backfile | 1950
|Calculation of downwash behind wings of arbitrary plan form at supersonic speeds
Engineering Index Backfile | 1950
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