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Robust Aerodynamic Design of Nacelles for Future Civil Aero-Engines
Robust Aerodynamic Design of Nacelles for Future Civil Aero-Engines
2020
B. Deneys J. Schreiner
Fernando Tejero
David G. MacManus
Christopher Sheaf
Keywords:
Thrust
Multi-objective optimization
Engineering
nitrogen oxides
Aviation
Aerodynamics
Aerospace engineering
Mach number
Nacelle
Design methods
Correction
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