Equations Flashcards
Theoretical drag
Dynamic pressure x surface area
p/2 x v^2 x A
Theoretical lift
Dynamic pressure x surface area
p/2 x v^2 x A
Coefficient of lift
Measured lift / theoretical lift
Coefficient of drag
Measured drag / theoretical drag
Actual lift
Coefficient of lift x dynamic pressure x surface area
Actual drag
Coefficient of drag x dynamic pressure x surface area
Lift to drag ratio
Best glide ratio
Coefficient of lift / coefficient of drag
Thrust
D + Wsin(theta)
Lift
Wcos(theta)
Taper ratio
Tip chord / root chord
Power
Work / time
Acceleration
Change of speed / time taken
Aspect ratio
Wing span / average chord
Work
Force x distance
Bernoulli’s equation
Ptot = p + q
Wing area
Wing span x chord
Speed
Distance / time
Continuity equation
V1 x A1 = V2 x A2
Mach number
Speed of the aircraft / speed of sound
Speed of sound
a = 20 x square root T
Pressure
Force / area
Dynamic pressure
q = p/2 x v^2
Force
Mass x acceleration
Weight
Mass x gravitational acceleration
Static pressure
Height x density x gravity