Labels:text | screenshot | multimedia software | software | display | graphics software OCR: CONTROL DIMENSIONS HIGH-LIFT DEVICES CHORD RATIO CONTROL DEFLECTION flap aileron (up/down) increase in stall angle caused by leading-edge devices (degrees) elevator or (up/down) Kruger flaps yield a 5 degree increase in stall angle. stabilator Slats provide an 8 degree increase in stall angle. CONTROL-EFFECTIVENESS APPROXIMATION rudder (degrees) wing has NON-FLUSH rivets, control surfaces are corrugated, and there are control-surface gaps roll spoiler (degrees) wing has FLUSH rivets, smooth control surfaces, but some control-surface gaps drag rudder (degrees) wing has FLUSH rivets, smooth control surfaces, and no control-surface gap. speedbrake (degrees)
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