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8SMS angle of 45 angle of attack aspect ratio body axes c.nfigurati.n C„.andCyvs CL Figure 27 CL vs CD Concluded CONF■GURAT■ON Q 3W45B CONF■GURAT■ON Q 5W50B CONFIGU0ATION 5W45B CONFIGU0ATION Q Continued curves more linear downstream panel downstream wing panel drooped-nose flaps Effect of drooped-nose equipped with drooped-nose Figure 11 Figure 28 flaps on downstream flow separation high lift coefficients i i i i i i i i iiii improve the linearity Krüger nose flaps L2ON llll llll llll TTTT low aspect-ratio low lift coefficients Mach number Moffett Field nose drooped 30 nose flaps mounted oblique wing equipped Root chord shown in figure static longitudinal characteristics sweep angle SYMBOL CONF■GURAT■ON SYMBOL CONFIGU0ATION 5W50B TTTT TTTT TTTT TTTTl unswept wing chord wing planform wing span yawing ТпТ