RCAIDE.Library.Methods.Aeroacoustics.Semi_Empirical.Airframe

Airframe

RCAIDE Package Setup

Modules

airframe_noise(microphone_locations, ...)	This computes the noise from different sources of the airframe for a given vehicle for a constant altitude flight.
clean_wing_noise(S, b, ND, IsHorz, velocity, ...)	This computes the 1/3 octave band sound pressure level and the overall sound pressure level from the clean wing.
landing_gear_noise(D, H, wheels, M, ...)	This calculates the Landing gear 1/3 octave band sound pressure level and overall sound pressure level.
trailing_edge_flap_noise(Sf, cf, deltaf, ...)	This calculates the noise from the flap trailing edge as a 1/3 octave band sound pressure level.