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13 Cards in this Set

  • Front
  • Back
p = m / v
Density= mass / volume
F = m • a
Force= mass • acceleration
P= W / t
Power= Work / time
W = F • s
Work= Force • (Distance of Displacement)
TE = PE + KE
Total Energy = Potential Energy + Kinetic Energy
PE = m • g • h
Potential Energy = mass • gravity • height

weight = m • g
KE = 1/2 • m • V^2
Kinetic Energy = 1/2 •mass • volume^2
M = F • d
Moment = Force • distance (from axis)
P = p • R • T
Pressure = density • R • Temperature

R = Constant for any Given Gas
S=bc
Wing Area = Wingspan x Average Chord
λ = C,T/C,R
Taper Ratio = Tip Chord / Root Chord
AR = b / c
Aspect Ratio = Wingspan / Average Chord
WL = W / S
Wing Loading = Weight of Airplane / Surface Area of Wings