Oblique wing aeroelasticity studies are reviewed. The static aeroelastic stability characteristics of oblique wing aircraft, lateral trim requirements for 1-g flight, and the dynamic aeroelastic stability behavior of oblique winged aircraft, primarily flutter, are among the topics studied. The similarities and differences between oblique winged aircraft and conventional, bilaterally symmetric, swept wing aircraft are emphasized.
An investigation of aeroelastic phenomena associated with an oblique winged aircraft
1976-08-31
Report
No indication
English
Aeroelastic Control of Oblique-Wing Aircraft
NTIS | 1986
|Aeroelastic control of oblique-wing aircraft
NTRS | 1986
|