The effects of aeroelasticity on stability and control are discussed under the two general categories of longitudinal and lateral motion. In each case the effects of wing, fuselage, and tail flexibility on stability of motion and effectiveness of control are considered for various flight conditions including dynamic pressure and Mach number. (Author)
Effects of Aeroelasticity on the Stability and Control Characteristics of Airplanes
1961
24 pages
Report
Keine Angabe
Englisch
Aerodynamics , Aircraft , Aeroelasticity , Jet aircraft , Airplanes , Stability , Flight control systems , Aerodynamic control surfaces , Ailerons , Tails (Aircraft) , Deflection , Deformation , Airframes , Structures , Mathematical analysis , Aerodynamic characteristics , Downwash , Aerodynamic loading , Roll , Flutter , Delta wings , Aerodynamic heating , Supersonic aircraft , Flexible structures , Fuselages , Canard configuration , Cpitch (Motion) , Transport aircraft , Jet fighters , Kernel functions , Piston theory , Supersonic transports
Effects of aeroelasticity on stability and control characteristics of airplanes
Engineering Index Backfile | 1961
|Aeroelasticity in Stability and Control
NTIS | 1957
FLIGHT VEHICLE AEROELASTICITY - Nonlinear Aeroelasticity
Online Contents | 2003
|