This paper presents the theoretically and practically grounded methods for aerodynamic compensation of aeroelastic divergence of a forward-swept wing. A special attention is paid to the discovered generation of a normally bound tornado-like vortex. Numerical research of separated flow morphology as well as lifting properties of the system are confirmed by a natural experiment in the wind tunnel and an in-flight experiment.
Aerodynamic Compensation Methods for Aeroelastic Divergence of Forward-Swept Wing
Russ. Aeronaut.
Russian Aeronautics ; 64 , 1 ; 28-36
01.01.2021
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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