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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 7
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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 7
Sizes of the different chimera grids used for 3D CFD performance evaluation.
Background: no droop nose
40,077,177 nodes
Background: with droop nose
72,109,161 nodes
Flaps
3,484,746 nodes