Annual report - National Advisory Committee for Aeronautics (1915)
United States. National Advisory Committee for Aeronautics · Washington, U.S. Govt. Print. Off · leaf 564
the flap deflected The effect of air speed or effective Reynolds Number would, no doubt, reduce the difference between the on the drag increment is shown in figure 26. The scale results with flap neutral and flap deflected. effect is much greater at high lift coefficients than at the The effect of… … 44. 12 5. 7 675. 0 125. 0 52.91 (». 45c _ Figure 32.— -Increase in drag due to slot-lip ailerons on the Fairchild 22 airplane in 6.3 No slot... ... 129.4 42. 75 772.5 51.37 the full-scale tunnel. Air speed, 56 m. p. h. slot-drag INVESTIGATION ACh against lift coefficient for the slot-lip ailerons…
Aeronautics · Aeronautics, Military · United States. National Advisory Committee for Aeronautics · Aeronautics -- United States -- Periodicals · Aeronautics, Military -- United States -- Periodicals
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