Originally Posted by
galaxy flyer
No, it’s not fixed. It will be less with compressibility effects or in ground effect. Different slat/flap configurations will also have effects, which is why I said narrow range of AoA. A 172 can be said to have a single stall AoA; gets more complicated with a wider range of configurations and conditions.
GF
Yes bowever i did recall saying provided the wing is clean i.e flaps up.
So my question again is. Is the stalling angle given for a specific aerofoil. Clean flaps up not dented no ive formed in ideal condition the same stalling angle?
Better still... what changes my stalling angle? Theres alot of talk about stalling speed and what affects it bur having an AOA Recorder i need to know if it is fixed or not