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Page Title:
Fig 5: Cause of Reduced T-45 Stability in Transonic Flight |
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|  T-45A/C TS, ADV & IUT Aero-02
High-Speed Flight
Wing
Horizontal Tail
Typical
Flow
Wing
Horizontal Tail
Resu
lt
Flow ant
Increased
Downwash
Figure 5: CAUSE OF REDUCED T-45 STABILITY IN TRANSONIC FLIGHT
(9-99) Original
Page 2-11
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