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To evaluate the aerodynamic and aeroacoustic feasibility of an advanced low-noise turboprop propeller concept designed to maintain high propulsive efficiency while limiting tip helical Mach number below 0.75 during cruise conditions.
by slilbaekslilbaek
82a845e4fda441 created this project
about 2 months ago
To evaluate the aerodynamic and aeroacoustic feasibility of an advanced low-noise turboprop propeller concept designed to maintain high propulsive efficiency while limiting tip helical Mach number below 0.75 during cruise conditions.