Unformatted text preview: ) position on the chord line. That is, ∞ − V V V lower upper . 2. Can you use results of part 1 to plot the difference between upper surface to lower surface pressure coefficients, ( ) lower p upper p c c , , − as a function of linear (not ) position on the chord line? Explain....
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- Fall '09
- Derivative, Airfoil, upper surface, chord line, Vlower, lower surface velocities