Last Updated：2025/11/25
When designing the slender fuselage, engineers applied the area rule to minimize transonic wave drag by matching the longitudinal cross-sectional area distribution to that of the Sears–Haack body.
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When designing the slender fuselage, engineers applied the area rule to minimize transonic wave drag by matching the longitudinal cross-sectional area distribution to that of the Sears–Haack body.
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