A theoretical investigation of the effect of yawing moment

Joseph L. Johnson, Leonard Sternfield
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.

An Adobe Acrobat (PDF) file of the entire report: