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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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┃ ┃- ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃
┃ ┃ ┃ ┃ ┃ ┃ 1 ┃ ┃ N ┃ ┃ ┃ ┃ ┃ ┃- ┃ ┃ ┃ ┃ ┃ ┃ ┃
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动力机械和机身手册1(108)
