Equations for Table:
q
=Â Â Â Â Â Â Â Â Â Â Â Â Â Â
CL =Â Â Â Â Â Â
CD = CDP + [1/ (e AR)] CL
2Â Â Â Â Â Â Â Â Â Â Â Â
Dp = CDp q S
Di = Dt - Dp = CDi q S = [1/ (e AR)] CL2 q
SÂ Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â Â
Dt = Di + Dp = CD q S
1.      Determine
VSTALLÂ Â Â Â Â Â Â Â (Stall speed
in KTAS)
Vstall = 150,64 KTAS
2.      Determine
DMINÂ Â Â Â Â Â Â Â Â Â Â Â Â Â (Minimum
drag in pounds)
Dmin = 461,54 lb
3.      Determine
VDMINÂ Â Â Â Â Â Â Â Â (Minimum
drag speed in KTAS)
Vdmin = 180 KTAS
4.      Determine the parasitic
drag at DMIN (pounds)
      DP min =219.78 lb
5.      Determine the induced drag
at DMIN (pounds)
Dimin = 241.76 lb
6.        Find Glide
Ratio at VDMIN
Glide Ratio = Cl/Cd = 21.67
