Unformatted text preview: x = 2 . 5 , 5 , 10 , 20 , 30 in along centerline (using hand-held pitot probe) 2) For α = 10 ◦ . . . Approximate locations where a) Δ p is a maximum (note the value) b) Δ p is a minimum (note the value) Normalized Data Presented 1) Top and bottom centerline C p vs x/c o for α = 0 ◦ , 10 ◦ . (both curves on one plot). Model’s centerline chord is c o = 37 . 7 in. 2) Locations of maximum and minimum Δ p , indicated with dots on the BWB outline drawing provided. Also determine the local normalized velocity V/V ∞ at these two locations. Note: Submit only the 2-sided turn-in sheet provided. If the plot is clearly incorrect, partial credit can be given only if you show your work (equations used, sample calculations, etc)....
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- Fall '05
- Wright brothers, Wing design, Chord, Pitot tube, blended wing body