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aircraft:tmd:airbrake

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aircraft:tmd:airbrake [2018/09/30 13:24] – [Example Code] jhaircraft:tmd:airbrake [2019/07/07 10:50] (current) – [Airbrake] jh
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 === Other Aerodynamic classes === === Other Aerodynamic classes ===
  
-[[aerowing]], [[airfoil]], [[aerofuselage]], [[propeller]], [[aerodrag]], [[bladeforce]]+[[aerowing]], [[airfoil]], [[aerofuselage]], [[propeller]], [[aerodrag]]
  
 ===== Function Description ===== ===== Function Description =====
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 Where Where
-  * The ''Body'' ([[rigidbody]]) velocity vector and the ''X0'' vector are multiplied using the vector dot product to find out how much the X0 axis of the airbrake is aligned with the current direction of flight. The norm (length) of the velocity (v) is multiplied by that dot product then squared.+  * is the velocity
   * Cd is the drag coefficient for the maximum ''Area''   * Cd is the drag coefficient for the maximum ''Area''
   * ''Area'' is the surface size in square meters perpendicular to X0.   * ''Area'' is the surface size in square meters perpendicular to X0.
aircraft/tmd/airbrake.txt · Last modified: 2019/07/07 10:50 by jh