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Modelling and Simulation in Engineering
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Modelling and Simulation in Engineering
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2011
/
Article
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Fig 19
/
Research Article
Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration
Figure 19
Comparison of
distribution (black line:
OPT1
, red line:
OPT2
).
(a)
32% semispan location
(b)
37% semispan location