Performance of Flight > Chapter 21: Turn > Flashcards
Centripetal Force Equation
CPF = MV^2/R
Load Factor Equation
n = 1 / cos(ϕ)
Turn Radius Equation
R = TAS^2 / ( g tan(ϕ) )
Rate of Turn Equation
RoT = 57.3 TAS / R °/s
Rate 1 Turn
3°/s
Rate 1 Turn Angle of Bank Equation
AoB = TAS / 10 + 7