An approximate spin design criterion for monoplanes, 1 May 1939
Description:
An approximate empirical criterion, based on the projected side area and the mass distribution of the airplane, was formulated. The British results were analyzed and applied to American designs. A simpler design criterion, based solely on the type and the dimensions of the tail, was developed; it is useful in a rapid estimation of whether a new design is likely to comply with the minimum requirements for safety in spinning.
Date:
January 1, 1976
Creator:
Seidman, O. & Donlan, C. J.
Item Type:
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UNT Libraries Government Documents Department