Pressure Distributions

Question 1

Draw the Cl vs AoA of neutral and cambered aerofoils.

Question 2

Draw the Cp vs x/c of neutral and cambered aerofoils.

Question 3

Draw the Cp vs x/c of a symmetrical centerline camber shape.

Question 4

Draw the Cl vs AoA of thin and thick aerofoils.

Question 5

Draw the Cd vs AoA of thin and thick aerofoils.

Question 6

Draw the Cp vs x/c of an aerofoil with no separation, LE separation and TE separation.

Question 7

Draw the Cp vs x/c of aerofoils exhibiting early and late transition.

Question 8

Draw the Cp vs x/c of a symmetric wing at an AoA.

Question 9

Draw the Cp vs x/c of a symmetric wing at an AoA with a TE flap.

Question 10

Draw the Cl vs AoA of a symmetric wing before and after adding a TE flap.

Question 11

Draw the Cp vs x/c of a symmetric wing at an AoA with a TE flap which has a GF.

Question 12

Draw the Cp vs y/s of a simple wing with and without endplates.

Question 13

Draw the Cd and Cl vs AoA of a simple wing with and without endplates.

Question 14

Draw the Cd vs AoA of short and long span wings.

Question 15

Draw the Cp vs x/L of an underbody in…
freestream
GE
GE with a diffuser
GE with a diffuser and RW

Question 16

Draw the Cp vs x/L of an entire car.