The Forces and Moments on Airplane Engine Mounts
Description:
"A resume of the equations and formulas for the forces and moments on an aircraft-engine mount is presented. In addition, available experimental data have been included to permit the computation of these forces and moments. A sample calculation is made and compared with present design conditions for engine mounts" (p. 1).
Date:
December 1936
Creator:
Donely, Philip
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department