Aerodynamic Moment#

The block calculates the aerodynamic moment component depending on the input factor.

Aerodynamic moment components are determined based on the ratios (1),(2) и (3) :

(1)#\[M_x=Q\cdot m_x\cdot S\cdot L\]

(2)#\[M_y=Q\cdot m_y\cdot S\cdot L\]

(3)#\[M_z=Q\cdot m_z\cdot S\cdot L\]

where:

Q - velocity head;

\(m_x, m_y, m_z\) - aerodynamic factors;

S - aerial device (AD) surface area;

L - length of aerial device.

1. Properties#

Property	Default Value	Description	Units of measurement
Aerial device (AD) surface area	0.2	-	m\(^2\)
Length of aerial device	1	-	m

Parameters	Input/Output	Description	Units of measurement	Port type
\(Sum_M\)	Input	Aerodynamic factor	-	Automation
Q	Input	Velocity head	N/m\(^2\)	Automation
M	Output	Aerodynamic Moment	N\(\cdot\)m	Automation

In order to see the connection capabilities of the block, you need to go to page Description of block ports