Enquiry
I am currently a SPL holder with 40hrs of flying at Malaysia.Currently at Navigation phase
I understand formula for lift is-->L=1/2 s*p*v*sq*Cl where Cl is coefficient lift,v is velocity of air,s is surface area of wing and p is density of air
I have to following question to ponder while revising my unusual attitude recovery
1)Why does increasing pitch decrease airspeed and why does decreasing pitch increases airspeed?
2)I understand when we are using aileron to turn,one wing lift is more than the other,hence we roll to either right/left