Investigations of the low speed longitudinal characteristics of two powered close coupled wing-canard fighter configurations are discussed. Data obtained at angles of attack from -2 deg to 42 deg, Mach numbers from 0.12 to 0.20, nozzle and flap deflections from 0 deg to 40 deg, and thrust coefficients from 0 to 2.0, to represent both high angle of attack subsonic maneuvering characteristics and conventional takeoff and landing characteristics are examined. Data obtained with the nozzles deflected either 60 deg or 90 deg and the flaps deflected 60 deg to represent vertical or short takeoff and landing characteristics are discussed.
Summary of low-speed longitudinal aerodynamics of two powered close-coupled wing-canard fighter configurations
1979-12-01
Report
Keine Angabe
Englisch
Effect of Canard Deflection on Close-Coupled Canard-Wing-Body Aerodynamics
Online Contents | 1994
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