What does MAC stand for in CG calculations?

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Multiple Choice

What does MAC stand for in CG calculations?

Explanation:
Mean Aerodynamic Chord is the reference length used in center of gravity calculations because it represents a single chord length that corresponds to the wing’s actual lift distribution. The MAC is defined as the chord length of a hypothetical wing segment that would produce the same total lift distribution as the real wing; it’s computed from the wing’s chord variation across the span (often shown as MAC = (2/S) ∫ c^2 dy). In CG work, the aircraft’s CG is commonly expressed as a percentage of the MAC, providing a consistent way to compare different wing geometries. The other terms aren’t standard in this context and don’t relate to how CG is tied to the wing’s lift characteristics.

Mean Aerodynamic Chord is the reference length used in center of gravity calculations because it represents a single chord length that corresponds to the wing’s actual lift distribution. The MAC is defined as the chord length of a hypothetical wing segment that would produce the same total lift distribution as the real wing; it’s computed from the wing’s chord variation across the span (often shown as MAC = (2/S) ∫ c^2 dy). In CG work, the aircraft’s CG is commonly expressed as a percentage of the MAC, providing a consistent way to compare different wing geometries. The other terms aren’t standard in this context and don’t relate to how CG is tied to the wing’s lift characteristics.

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