There are three lateral dynamic attitudes, delineated by rolling, yawing, and sideslipping. It is possible to solve for the pressures on the rolling wing by quasi‐steady analysis. This approach is, however, inapplicable for the yawing or sideslipping wing, and it is with the latter two cases that this paper deals.
(1955), "Institute of the Aeronautical Sciences Annual Meeting: Summaries of Papers Presented to the 23rd Annual General Meeting Held in New York on January 24–27, 1955", Aircraft Engineering and Aerospace Technology, Vol. 27 No. 4, pp. 117-124. https://doi.org/10.1108/eb032544
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