RCAIDE.Library.Methods.Aeroacoustics.Semi_Empirical.Turbofan.angle_of_attack_effect.angle_of_attack_effect#

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_metric

https://example.com/A_weighting_metric

RCAIDE.Library.Methods.Aeroacoustics.Common.SPL_arithmetic

https://example.com/SPL_arithmetic