Drag polar 0.8 0.6 0.4 0.2 0.5 1.5 2 2.5 3 Coefficient of lift(Cl) Re-5003352 Coefficient of drag(Cd) 1.
Drag polar 0.8 0.6 0.4 0.2 0.5 1.5 2 2.5 3 Coefficient of lift(Cl) Re-5003352 Coefficient of drag(Cd) 1.
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Comment on the drag polar for both the shapes
Transcribed Image Text:Drag polar
8 0.8
0.6
0.4
0.2
0.
0.5
1.5
2.5
3.
Coefficient of lift(Cl)
Re-5003352
FIGURE 2.3-DRAG POLAR FOR ASYMMETRICAL AIRFOIL
2.
1.
Coefficient of drag(Cd)
Transcribed Image Text:Drag polar
0.3
0.2
0.1
0.5
1
1.5
Coefficient of lift(Cl)
Re-5003352
FIGURE 3.3- DRAG POLAR FOR FLAT PLATE
Coefficient of drag(Cd)
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