Analysis of the effects of wing interference on the tail contributions to the rolling derivatives
Description:
From Introduction: "This report presents calculations of the angularity of the air stream with respect to the vertical tail for a rolling airplane, the interference effects of the wing being taken into account. A discussion of the factors which enter into the calculations is given and equations for applying the side-wash results to the determination of the tail contributions to the rolling-stability derivatives are included. The results are compared with some available experimental data."
Date:
January 24, 1951
Creator:
Michael, William H., Jr.
Item Type:
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