aircraft:tmd:airbrake
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aircraft:tmd:airbrake [2017/01/23 23:10] – jh | aircraft:tmd:airbrake [2019/07/07 10:50] (current) – [Airbrake] jh | ||
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=== Other Aerodynamic classes === | === Other Aerodynamic classes === | ||
- | [[aerowing]], | + | [[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 '' | ||
+ | |||
+ | ===== Example Code ===== | ||
+ | > **Caution**: | ||
+ | |||
+ | < | ||
+ | < | ||
+ | < | ||
+ | < | ||
+ | < | ||
+ | < | ||
+ | < | ||
+ | ></ | ||
aircraft/tmd/airbrake.1485209402.txt.gz · Last modified: 2017/01/23 23:10 by jh