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Modelling and Simulation in Engineering
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Modelling and Simulation in Engineering
/
2011
/
Article
/
Tab 3
/
Research Article
Aerodynamic Optimization of an Over-the-Wing-Nacelle-Mount Configuration
Table 3
Pylon thickness and
for two optimal solutions (
OPT1
and
OPT2
).
OPT1
OPT2
Pylon thickness
8.0%
9.0%
34.5
35.5