Secondary effects in static aeroelasticity that heretofore have been regarded as negligble include: redistribution of induced drag; dihedral effect under load factor; structural axis rotations in equations of motion; aeroelastic divergence of an unrestrained vehicle; and corrections to measurements on 'rigid' wind tunnel model. The few publications on these topics that have appeared over the years are surveyed on the assumption that secondary effects on earlier designs may have become primary effects of future configurations.
Secondary Considerations of Static Aeroelastic Effects on High-Performance Aircraft
1986
13 pages
Report
No indication
English
Static aeroelastic effects on high-performance aircraft
TIBKAT | 1986
|Some static aeroelastic considerations of slender aircraft
Engineering Index Backfile | 1961
|