Recent content by ajf

Thanks for your replies - Yes, I am far from happy with my understanding, my regular teacher is absent just now, and the cover teacher specialises in other subjects. I have put a value of air density of 1.252kg /cubic metre into the equation and things have made a bit more sense. (The...

I have done a lab experiment, to determine the coefficient of lift for an aerofoil, keeping the angle of attack constant. The equation I have used is Lift= (1/2) v times v times A times ρ times Coefficient of lLift v= Velocity of air ρ=air density A= planform area to give...