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13 Cards in this Set
- Front
- Back
p = m / v
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Density= mass / volume
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F = m • a
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Force= mass • acceleration
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P= W / t
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Power= Work / time
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W = F • s
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Work= Force • (Distance of Displacement)
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TE = PE + KE
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Total Energy = Potential Energy + Kinetic Energy
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PE = m • g • h
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Potential Energy = mass • gravity • height
weight = m • g |
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KE = 1/2 • m • V^2
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Kinetic Energy = 1/2 •mass • volume^2
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M = F • d
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Moment = Force • distance (from axis)
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P = p • R • T
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Pressure = density • R • Temperature
R = Constant for any Given Gas |
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S=bc
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Wing Area = Wingspan x Average Chord
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λ = C,T/C,R
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Taper Ratio = Tip Chord / Root Chord
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AR = b / c
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Aspect Ratio = Wingspan / Average Chord
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WL = W / S
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Wing Loading = Weight of Airplane / Surface Area of Wings
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