The experimental and analytical techniques used in free rolling motion of vehicles are summarized. The flight dynamics at significant angles of attack are discussed in relation to nonlinear aerodynamic characteristics and pitch-yaw-roll coupling. The problem of nonoscillatory free-flight motion analysis is addressed. Equations for roll data reduction applicable to aircraft configurations are presented.
Rolling Motion of Canard Missiles in Wind Tunnel Free-Flight Tests
1978
32 pages
Report
Keine Angabe
Englisch
Missile Technology , Aerodynamics , Canard configurations , Missiles , Rolling moments , Free flight test apparatus , Wind tunnel tests , Aerodynamic characteristics , Aircraft configurations , Angle of attack , Damping , Data reduction , Flight tests , Nonlinear equations , Oscillations , Pitch(Inclination) , Roll , Yaw , South Africa
Free-spinning-tunnel tests of model of canard airplane
Engineering Index Backfile | 1943
|