By application of semirigid analysis divergence speed coefficient is obtained in form of two factors involving modes of deformation and downwash; results in case of normal plain wings are illustrated by curves of divergence speed factor as function of taper ratio.
Estimation of wing torsional divergence speed with downwash correction
Nat Research Council Canada -- Aeronautical Note
1948
7 pages
2 supp p
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Downwash correction for a two-dimensional finite wing
AIAA | 1971
|Calculation of downwash behind wing
Engineering Index Backfile | 1938
|Prediction of downwash behind swept-wing airplanes at subsonic speed
Engineering Index Backfile | 1955
|The Downwash Field behind a swept wing at low speed
TIBKAT | 1968
|