Effects of wing leading-edge flap deflections on subsonic longitudinal aerodynamic characteristics of a wing-fuselage configuration with a 44° swept wing
NASA technical paper ; 1351
1978
35 S.
Ill., graph. Darst.
Langzeitarchivierung durch Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
Englisch
Aerodynamic Design of Swept Infinite Wing with Flap for Subsonic and Transonic Flight Regimes
British Library Online Contents | 1996
|