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Unformatted text preview: 50 mph Angles of attack: = , 5 , 10 , 15 Raw Data Acquired p , p o (from tunnels pitot-static probe) p ( x ) , p o ( x ) (along nose centerline, using hand-held pitot probe) Lift, Drag (from tunnel balance) Normalized Data Presented Top and bottom centerline C p ( x ) for each . (All 8 curves on one plot) C L ( ), C D ( ) Analysis Propose locations of static ports on centerline, and how their measured p s could be used to best estimate p and hence V for any . You may assume that p o is known accurately on the aircraft (since this is easy to measure)....
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