Inheritance diagram for SUAVE.Components.Nacelles.Nacelle.Nacelle:

Public Member Functions
def	__defaults__ (self)

def	append_segment (self, segment)

def	append_airfoil (self, airfoil)

def	nac_vel_to_body (self)

def	body_to_nac_vel (self)

def	vec_to_vel (self)

Public Attributes
	tag

	origin

	aerodynamic_center

	areas

	diameter

	inlet_diameter

	length

	orientation_euler_angles

	flow_through

	differential_pressure

	Airfoil

	cowling_airfoil_angle

	Segments

Public Attributes inherited from SUAVE.Components.Lofted_Body.Lofted_Body
	tag

	Segments

Public Attributes inherited from SUAVE.Components.Physical_Component.Physical_Component
	tag

	mass_properties

	origin

	symmetric

Public Attributes inherited from SUAVE.Components.Component.Component
	tag

	origin

	generative_design_max_per_vehicle

	generative_design_characteristics

	generative_design_special_parent

Detailed Description

This is a nacelle for a generic aircraft.

Assumptions:
None

Source:
N/A

Member Function Documentation

◆ defaults()

def SUAVE.Components.Nacelles.Nacelle.Nacelle.__defaults__ ( self )

This sets the default values for the component to function.

Assumptions:
None
    
Source:
N/A
    
Inputs:
None
    
Outputs:
None
    
Properties Used:
None

Reimplemented from SUAVE.Components.Lofted_Body.Lofted_Body.

◆ append_airfoil()

def SUAVE.Components.Nacelles.Nacelle.Nacelle.append_airfoil	(	self,
		airfoil
	)

Adds an airfoil to the segment 
    
Assumptions:
None

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
N/A

◆ append_segment()

def SUAVE.Components.Nacelles.Nacelle.Nacelle.append_segment	(	self,
		segment
	)

Adds a segment to the nacelle. 
    
Assumptions:
None
Source:
N/A
Inputs:
None
Outputs:
None
Properties Used:
N/A

◆ body_to_nac_vel()

def SUAVE.Components.Nacelles.Nacelle.Nacelle.body_to_nac_vel ( self )

This rotates from the systems body frame to the nacelles velocity frame

Assumptions:
There are two nacelle frames, the vehicle frame describing the location and the nacelle velocity frame
velocity frame is X out the nose, Z towards the ground, and Y out the right wing
vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
None

◆ nac_vel_to_body()

def SUAVE.Components.Nacelles.Nacelle.Nacelle.nac_vel_to_body ( self )

This rotates from the systems body frame to the nacelles velocity frame

Assumptions:
There are two nacelle frames, the vehicle frame describing the location and the nacelle velocity frame
velocity frame is X out the nose, Z towards the ground, and Y out the right wing
vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
None

◆ vec_to_vel()

def SUAVE.Components.Nacelles.Nacelle.Nacelle.vec_to_vel ( self )

This rotates from the nacelles vehicle frame to the nacelles velocity frame

Assumptions:
There are two nacelle frames, the vehicle frame describing the location and the nacelle velocity frame
velocity frame is X out the nose, Z towards the ground, and Y out the right wing
vehicle frame is X towards the tail, Z towards the ceiling, and Y out the right wing

Source:
N/A

Inputs:
None

Outputs:
None

Properties Used:
None

The documentation for this class was generated from the following file:

/Users/emiliobotero/Dropbox/SUAVE/SUAVE/trunk/SUAVE/Components/Nacelles/Nacelle.py

Public Member Functions

Public Attributes