HWD -
Stall is only a function of AoA
I beg to differ from that statement, without wishing to start an argument. IIRC, stall speed is a function of:
- Wing Loading (A/c Weight)
- Aerofoil Section (inluding whether additional lift devices, such as flaps, or if spoilers, are deployed)
- Any icing / surface degradation (such as flies / dents) on the mainplane
- A of A
- Manoeuvering Loads
- Air Temp / Density
Whilst a typical wing under typical conditions may stall at around 15 deg A of A, this is not an absolute figure.