The results were determined as a function of values at the wing trailing edge and at the Trefftz-plane. A correction for off the wing plane points is given. A description of the method, a FORTRAN listing of the coded method and results to be compared with theoretical and experimental values of downwash are presented.
Downwash Calculation at Close Range Behind a Trapezoidal Wing in Supersonic Flow
1980
37 pages
Report
Keine Angabe
Englisch
Calculation of downwash behind wing
Engineering Index Backfile | 1938
|Charts for estimating downwash behind rectangular, trapezoidal, and triangular wings at supersonic
Engineering Index Backfile | 1950
|