RCAIDE.Library.Methods.Noise.Correlation_Buildup.Turbofan.angle_of_attack_effect.angle_of_attack_effect

angle_of_attack_effect(AoA, Mach_aircraft, theta_m)

This calculates the angle of attack effect, in decibels, to be added to the predicted mixed jet noise level.

Assumptions:

N/A

Source:

SAE Model

Inputs:

AoA angle of attack [rad] Mach_aircraft mach number of aircraft [Unitless] theta_m emission angle [rad]

Outputs:

ATK_m angle of attack effect [Unitless]

Properties Used:

None