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If an aircraft has lift curve slope of 4.76 per rad and moment coefficient curve slope of -0.116 per rad then, find the location of neutral point. Consider Xcg=0.3.

Correct Answer: 0.324
Location of neutral point = Xcg – moment coefficient slope/lift curve slope = 0.3 – 0.116/4.76 = 0.3-0.024 = 0.324.

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