Differences

This shows you the differences between two versions of the page.

--- aircraft:tmd:airfoil [2018/09/30 13:21] – [ClAlpha] jh
+++ aircraft:tmd:airfoil [2019/07/07 10:49] – [Airfoil] jh
@@ Line 4: / Line 4: @@
 === Other Aerodynamic classes ===
-[[aerowing]], [[aerofuselage]], [[airbrake]], [[propeller]], [[aerodrag]], [[bladeforce]]
+[[aerowing]], [[aerofuselage]], [[airbrake]], [[propeller]], [[aerodrag]]
 ===== Angle of attack =====
@@ Line 127: / Line 127: @@
 ''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 }}