An aircraft is described with a single fuselage having a main wing and a horizontal stabilizer airfoil pivotally attached at their centers to the fuselage. The pivotal attachments allow the airfoils to be yawed relative to the fuselage for high speed flight, and to be positioned at right angles with respect to the fuselage during take-off, landing, and low speed flight. The main wing and the horizontal stabilizer are upwardly curved from their center pivotal connections towards their ends to form curvilinear dihedrals.
Single Wing Supersonic Aircraft
1973
39 pages
Report
Keine Angabe
Englisch
Single Wing Supersonic Aircraft
NTIS | 1974
|Oblique-wing supersonic aircraft
NTRS | 1976
|Extremely-simple supersonic flying wing layout aircraft
Europäisches Patentamt | 2021
|Flutter calculations on a supersonic aircraft wing
TIBKAT | 1957
|