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aircraft:tmd:airfoil

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aircraft:tmd:airfoil [2018/09/30 13:21] – [ClAlpha] jhaircraft:tmd:airfoil [2019/07/07 10:35] – [CmAlphaBase] jh
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 ''ClAlphaBase'' is usually the maximum momentum coefficient an airfoil will ever create. ''ClAlphaBase'' is usually the maximum momentum coefficient an airfoil will ever create.
  
-> The lower the value of ''ClAlphaBase'' the more the nose will drop when approaching a stall. Values near ''-0.2'' tend to soften the stall behavior. +> The lower the value of ''CmAlphaBase'' the more the nose will drop when approaching a stall. Values near ''-0.2'' tend to soften the stall behavior. 
  
 {{ Airfoil_Stall_ClAlphaBase.png?nolink }} {{ Airfoil_Stall_ClAlphaBase.png?nolink }}
aircraft/tmd/airfoil.txt · Last modified: 2020/09/28 22:44 by jh