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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2019
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Article
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Tab 6
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Research Article
Aerodynamic Shape Design and Validation of an Advanced High-Lift Device for a Regional Aircraft with Morphing Droop Nose
Table 6
Flap setting for the high-lift conditions.
Final settings
LDG
TO
Deflection
35 deg
20 deg
Gap/chord
2.16%
2.26%
Overlap/chord
-0.25%
-0.43%