aircraft:tmd:airbrake
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aircraft:tmd:airbrake [2017/01/23 23:09] – created jh | aircraft:tmd:airbrake [2019/07/07 10:50] (current) – [Airbrake] jh | ||
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In the Aerofly FS 2 an '' | In the Aerofly FS 2 an '' | ||
+ | |||
+ | === Other Aerodynamic classes === | ||
+ | |||
+ | [[aerowing]], | ||
===== Function Description ===== | ===== Function Description ===== | ||
The airbrake is probably using something similar to this formula: | The airbrake is probably using something similar to this formula: | ||
- | < | + | < |
Where | Where | ||
- | * The '' | + | * v is the velocity |
* Cd is the drag coefficient for the maximum '' | * Cd is the drag coefficient for the maximum '' | ||
* '' | * '' | ||
* '' | * '' | ||
* '' | * '' | ||
+ | * rho is the air density at the Body.R position in the world (+R0 properly rotated with the Body orientation as far as the author of this text wants to believe) | ||
+ | Then the calculated drag is acted upon the '' | ||
- | === Other Aerodynamic classes | + | ===== Example Code ===== |
+ | > **Caution**: | ||
- | [[aerowing]], [[airfoil]], [[aerofuselage]], [[propeller]], [[aerodrag]], [[bladeforce]], [[bodyaerodynamics]] | + | < |
+ | <[string8][Body][Fuselage]> | ||
+ | <[tmvector3d][R0][ 0.0 0.0 0.0 ]> | ||
+ | <[tmvector3d][X0][ 1.0 0.0 0.0 ]> | ||
+ | <[float64][Cd][1.5]> | ||
+ | <[float64][Area][1.0]> | ||
+ | <[string8][Control][ServoAirbrake.Output]> | ||
+ | ></ | ||
aircraft/tmd/airbrake.txt · Last modified: 2019/07/07 10:50 by jh