RCAIDE.Library.Methods.Aeroacoustics.Semi_Empirical.Turbofan.angle_of_attack_effect
angle_of_attack_effect#
Functions
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This module predicts the free-field 1/3 Octave Band Sound Pressure Level (SPL) of coaxial subsonic jets for turbofan engines. |
- angle_of_attack_effect(AoA, Mach_aircraft, theta_m)[source]#
This module predicts the free-field 1/3 Octave Band Sound Pressure Level (SPL) of coaxial subsonic jets for turbofan engines. It uses semi-empirical methods to account for various conditions such as flyover, static, and in-flight scenarios.
See also
RCAIDE.Library.Methods.Aeroacoustics.Metrics.A_weighting_metricRCAIDE.Library.Methods.Aeroacoustics.Common.SPL_arithmetic