Discuss and comment on the effect of drag polar for Re 5003352. Drag polar6.50.40.30.20.10.511.5Coefficient of lift(Cl)- Re=50074- Re=500995- Re=5003352FIGURE 1.3- DRAG POLAR FOR SYMMETRICAL AIRFOILCoefficient of drag(Cd) Drag polar0.80.60.40.20.511.522.5Coefficient of lift(CI)Re=5003352Re=50074Re=500995FIGURE 2.3- DRAG POLAR FOR ASYMMETRICAL AIRFOIL3.1.Coefficient of drag(Cd)

The lift-to-drag proportion increments as Reynolds number increments for both the airfoils…

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Discuss and comment on the effect of drag polar for Re 5003352

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

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Question

Discuss and comment on the effect of drag polar for Re 5003352.

Drag polar
6.5
0.4
0.3
0.2
0.1
0.5
1
1.5
Coefficient of lift(Cl)
- Re=50074
- Re=500995
- Re=5003352
FIGURE 1.3- DRAG POLAR FOR SYMMETRICAL AIRFOIL
Coefficient of drag(Cd)

Drag polar
0.8
0.6
0.4
0.2
0.5
1
1.5
2
2.5
Coefficient of lift(CI)
Re=5003352
Re=50074
Re=500995
FIGURE 2.3- DRAG POLAR FOR ASYMMETRICAL AIRFOIL
3.
1.
Coefficient of drag(Cd)

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