POF Equations Flashcards
1
Q
Load factor equation
A
Lift/weight
2
Q
Equation for AR
A
AR = Span^2/ wing area
3
Q
% of Cl Max
A
CL= 1/new Vs^2
4
Q
Induced drag and IAS
A
Proportional to 1 / IAS^2
5
Q
Ground effect noticeable when
A
1/2 wingspan
6
Q
Stall speed in a turn
A
Stall speed level x (Root 1/cos angle)
7
Q
What happens to stall speed when high lift devices increase Clmax
A
Vs decreases to maintain same amount of lift
8
Q
Load factor and stall speed
A
New stall speed = Vs x (root load factor)
