Discussion of rapid approximation method, so-called superposition method, to calculate aeroelastic wing deformations; reliability of method proved by comparing numerical results with those reached by more exact method.
Influence of aeroelastic distortion on static longitudinal stability of airplanes with sweptback wings
Invloed van de aeroelasticiteit op de langsstabiliteit
Ingenieur ; 69 , n 23
1957
Aufsatz (Zeitschrift)
Niederländisch
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Static longitudinal stability of "Ente" airplanes
NTRS | 1931
|Static longitudinal stability of "Ente" airplanes
TIBKAT | 1931
|Static longitudinal stability of "Ente" airplanes
Engineering Index Backfile | 1930
|