aircraft:tmd:airbrake
Differences
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Both sides previous revisionPrevious revisionNext revision | Previous revision | ||
aircraft:tmd:airbrake [2017/01/23 23:13] – 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 ===== | ||
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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 '' | Then the calculated drag is acted upon the '' | ||
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===== Example Code ===== | ===== Example Code ===== | ||
> **Caution**: | > **Caution**: | ||
- | | + | |
- | <[string8][Name][Airbrake]> | + | <code> |
- | < | + | < |
- | < | + | < |
- | < | + | < |
- | < | + | < |
- | < | + | < |
- | < | + | < |
- | > | + | ></ |
aircraft/tmd/airbrake.1485209620.txt.gz · Last modified: 2017/01/23 23:13 by jh