A theoretical investigation of the effect of yawing moment

Joseph L. Johnson, Leonard Sternfield
naca-tn-1723
Oct 1948


due to rolling on lateral oscillatory stability The effect on lateral oscillatory stability of varying the value of stability derivative Cnp (yawing-moment coefficient due to rolling-angular-velocity factor) over a wide range of negative and positive values has been determined theoretically for a sweptback fighter airplane with loading conditions simulating an airplane with wing-tip fuel tanks and without wing-tip fuel tanks.

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