WIND TUNNEL EXPERIMENTAL PROCEDURE
MAE 175A Wind TUNNEL Experiment (K. Seshadri) Written by Cattolica, modified by Tynan 1/10/2014 11WIND TUNNEL EXPERIMENTAL PROCEDURE MAE 175A PART I Pressure Distribution over an airfoil and Drag by the wake survey method OBJECTIVE: Measure the pressure distribution over a Clark Y-14 Airfoil at various angles of attack and determine the drag coefficient of the wing by the wake survey method. Data are obtained up to and beyond the stall angle, where the flow separates from the upper surface of the airfoil. INTRODUCTION: An airfoil develops Lift through generally lower pressures above the wing and higher below with respect to the pressure of the approaching air.
Jan 10, 2014 · 10, 20, 30, 40, 50, 60 and 70 percent chord on both upper and lower surfaces and there is an additional opening at 80 percent chord on the upper surface. To complete the pressure distribution you should extrapolate the last measurements on the upper and lower surfaces of the wing to a ... system by q ∞ gives the ...
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