In theory, the most efficient wing shape for transonic and low supersonic speeds is simply a long narrow straight subsonic wing turned at an oblique angle to the flight direction. This theory has been verified by tests at Mach numbers from .6 to 1.4 in supersonic wind tunnel and by comparative studies of transonic transport designs.
Aeroelastic characteristics of an oblique wing
01.02.1976
Sonstige
Keine Angabe
Englisch
Aeroelastic control of oblique-wing aircraft
NTRS | 1986
|Aeroelastic Control of Oblique-Wing Aircraft
NTIS | 1986
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