Spinning Characteristics of Wings IV : Changes in Stagger of Rectangular Clark Y Cellules (1937)
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-5 0 5 10 15 SO .25 . 50 . 75 1.00 Angle f sideslip, P ,deg. Figure 4.- Variation of rolling-moment ooefficiont C, (body axes) with angle of sideelip and ^b/2V.
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