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WIND TUNNEL EXPERIMENTAL PROCEDURE

WIND TUNNEL EXPERIMENTAL PROCEDURE

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Jan 10, 2014 · This method of drag measurement is often used on portions of airplane wings in flight to test special drag profiles or surface treatments. The pitching moment can also be obtained from the chordwise pressures by use of (Ref. 1) Cm LE = 1 c2 ∆P ∫q (x)dc where:x = distance from leading edge (or other selected reference point). PROCEDURE: 1.

  Measurement, Procedures

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