SUAVE  2.5.2
An Aerospace Vehicle Environment for Designing Future Aircraft
Certification

Functions

def SUAVE.Methods.Noise.Certification.approach_noise.approach_noise (analyses, noise_configs)
 
def SUAVE.Methods.Noise.Certification.flyover_noise.flyover_noise (analyses, noise_configs)
 
def SUAVE.Methods.Noise.Certification.sideline_noise.sideline_noise (analyses, noise_configs)
 

Detailed Description

Function Documentation

◆ approach_noise()

def SUAVE.Methods.Noise.Certification.approach_noise.approach_noise (   analyses,
  noise_configs 
)
This method calculates approach noise of a turbofan aircraft
        
Assumptions:
    N/A

Source:
    N/A 

Inputs:
    analyses        - data structure of SUAVE analyses                [None]
    noise_configs   - data structure for SUAVE vehicle configurations [None]

Outputs: 
    SPL             - sound pressure level                            [dB]

Properties Used:
    N/A 

◆ flyover_noise()

def SUAVE.Methods.Noise.Certification.flyover_noise.flyover_noise (   analyses,
  noise_configs 
)
This method calculates flyover noise of a turbofan aircraft
        
Assumptions:
    N/A

Source:
    N/A 

Inputs:
    analyses        - data structure of SUAVE analyses                [None]
    noise_configs   - data structure for SUAVE vehicle configurations [None]

Outputs: 
    SPL             - sound pressure level                            [dB]

Properties Used:
    N/A 

◆ sideline_noise()

def SUAVE.Methods.Noise.Certification.sideline_noise.sideline_noise (   analyses,
  noise_configs 
)
This method calculates sideline noise of a turbofan aircraft
        
Assumptions:
    N/A

Source:
    N/A 

Inputs:
    analyses        - data structure of SUAVE analyses                [None]
    noise_configs   - data structure for SUAVE vehicle configurations [None]

Outputs: 
    SPL             - sound pressure level                            [dB]

Properties Used:
    N/A