曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Just as wing affects the fuselage flow field, fuselage induces a crossflow that affects
the spanwise lift distribution over the wing. The fuselage interference effects on
the wing are generally small for configurations with large wing-span-to-body-
diameter ratios typified by conventional long-range subsonic airplanes. For such
configurations, lift-curve slope of the wing in the presence of the fuselage can be
assumed to be equal to that of an isolated wing.
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STATIC STABILITY AND CONTROL
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