Low-speed stability and control wind-tunnel investigation of effects of spanwise blowing on fighter flight characteristics at high angles of attack
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adverse yawing aerodynamic data aft port location aileron effectiveness angle of attack angle-of-attack range asymmetric blowing asymmetric spanwise blowing attack of 30 blowing rate control characteristics current fighter airplane deg Figure delta wing planform due to spanwise dynamic lateral-directional stability dynamic pressure effects of blowing effects of spanwise figure 28 flight characteristics flight tests flow visualization free-flight tests fuselage improved influence of spanwise Langley Research Center LCDP leading-edge vortex lift augmentation ratio lift coefficient lift-to-drag ratio mean aerodynamic chord mentation NASA TN pitch presented in figure range from 15 reattachment refs roll damping rudder effectiveness shown in figure spanwise-blowing port spanwise-blowing thrust coefficient stability and control stability derivatives static force tests static lateral-directional characteristics static longitudinal characteristics tests were conducted trape trapezoidal wing Tunnel U.S. Customary Units vertical tail vertical-tail effectiveness Vortex Lift wing leading edge wing rock wise blowing zoidal wing