Quadratic synthesis of integrated active controls for an aeroelasticforward-swept-wing-aircraft
Guidance and Control Conference ; 1982 ; San Diego , CA , U.S.A.
1982-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
High performance forward swept wing aircraft
NTRS | 1988
|High Performance Forward Swept Wing Aircraft
NTIS | 1986
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