A study of the pitching moments and the stability characteristics of monoplanes (1934)
NASA Technical Reports Server (NTRS) · leaf 23
-.0012 Effective aspect ratio of wing, Aw Figure 12.- Effect of different variables on the -.0016 stability coefficient. Figure 13.- The effect of filleting on the lift and ving monoplane. a,hypothetical low-wing airplane. b, low-wing airplane with burbling effects, c, low-wing airplane with…
NASA Technical Reports Server (NTRS)
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