Engee documentation

Aerodynamic Forces and Moments

Calculation of aerodynamic forces and moment.

blockType: SubSystem

Path in the library:

/Aerospace/Aerodynamics/Aerodynamic Forces and Moments

Description

Block Aerodynamic Forces and Moments calculates the components of the aerodynamic force and the aerodynamic moment relative to the center of gravity of the aircraft in the associated coordinate system using the following formulas.

Components of the aerodynamic force:

where

  • — coefficient of longitudinal force;

  • — the coefficient of normal force;

  • — coefficient of lateral force;

  • — high-speed pressure;

  • — a characteristic square.

Components of the aerodynamic moment:

where

  • — roll moment coefficient;

  • — coefficient of yaw moment;

  • — the coefficient of pitch moment;

  • — the characteristic linear size of the aircraft;

  • — the average aerodynamic chord of the wing;

  • , , — coordinates of the center of gravity;

  • , , — coordinates of the pressure center.

Ports

Input

# Coefficientsdescription missing

Details

Description missing

Data types

Description missing

Complex numbers support

Description missing

# qbardescription missing

Details

Description missing

Data types

Description missing

Complex numbers support

Description missing

# CG — centre of gravity coordinates
`vector 3 to 1

Details

The coordinates of the centre of gravity of an aircraft. Measured in units of length, given as a vector.

Data types

Float64.

Complex numbers support

No

# CP — centre of pressure coordinates
`vector 3 to 1

Details

The coordinates of the centre of pressure of an aircraft, given as a vector. Measured in units of length.

Data types

Float64.

Complex numbers support

No

Output

# Forcesdescription missing

Details

Description missing

Data types

Description missing

Complex numbers support

Description missing

# Momentsdescription missing

Details

Description missing

Data types

Description missing

Complex numbers support

Description missing

Parameters

Main

# Reference area — characteristic area

Details

The characteristic area of an aircraft. It is measured in units of area. For aircraft, the wing area is usually taken as the characteristic area.

Default value

1.0

Program usage name

S

Tunable

No

Evaluatable

Yes

# Reference span — mean aerodynamic chord of the wing

Details

The average aerodynamic chord of a wing. Measured in units of length.

Default value

1.0

Program usage name

b

Tunable

No

Evaluatable

Yes

# Reference length — characteristic linear dimension

Details

The characteristic linear dimension of an aircraft. It is measured in units of length. For aircraft, the characteristic linear dimension is usually taken as the wingspan.

Default value

1.0

Program usage name

cbar

Tunable

No

Evaluatable

Yes