Effects of wing, fuselage, and tail flexibility on stability of motion and effectiveness of control are discussed for various flight conditions including dynamic pressure and Mach number; review of problems, such as reduced roll damping and aileron reversal, and extent to which they appear in recent designs of fighters, bombers, transports; features incorporated to reduce adverse aeroelastic effects on stability and control; results from studies of supersonic transport and winged missile.
Effects of aeroelasticity on stability and control characteristics of airplanes
AGARD -- Report
1961
29 pages
Report
English
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Aeroelasticity in Stability and Control
NTIS | 1957
FLIGHT VEHICLE AEROELASTICITY - Nonlinear Aeroelasticity
Online Contents | 2003
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