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Page Title:
Fig 3: Effect of Geometric Twist, Flaps, and Slats |
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|  T-45A/C TS, E2-C2, ADV & IUT Aero-03
Slow-Speed Flight, Stall and Spin, and AOA System
Constant
Incidence
Wing
CL
AOA in Degrees
3 1/2
CL
AOA in Degrees
CL
AOA in Degrees
Figure 3: EFFECT OF GEOMETRIC TWIST, FLAPS, AND SLATS
(9-99) Original
Page 3-7
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