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Stability about yawing axis is called as __________(a) directional stability(b) lateral stability(c) longitudinal stability(d) pitching moment stabilityThe question was posed to me in examination.My doubt is from Lateral-Directional Static Stability and Control in chapter Stability, Control, and Handling Qualities of Aircraft Design

Answer»

The correct ANSWER is (a) directional stability

The best explanation: Directional stability of the AIRCRAFT is defined as the stability about the yawing axis. In typical aircraft yaw and rolling both will be PRODUCED by DEFLECTING the rudder. Stability about rolling moment is called lateral stability.



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