7. Consider the Vorticity distribution 1+ cose r(0) = 2aU, sine Calculate the section pitching moment about a point 0.75 chord from the leading edge. Note that you can use the fact that the center of pressure (Xcp) is at the quarter chord for all angles of attack, as well as the definition for lift.
7. Consider the Vorticity distribution 1+ cose r(0) = 2aU, sine Calculate the section pitching moment about a point 0.75 chord from the leading edge. Note that you can use the fact that the center of pressure (Xcp) is at the quarter chord for all angles of attack, as well as the definition for lift.
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