Force- and Pressure-Distribution Measurements on Eight Fuselages
Description:
"The present report deals with force- and pressure-distribution measurements on a number of fuselage forms of varying slenderness ratio, varying rearward position of maximum thickness, and varying nose ratio. The effect of these parameters on the force and moment coefficients was determined. The linearity of the difference between the theoretical and experimental fuselage moments with the friction lift made it possible to indicate a neutral point and its travel with the different parameters" (p…
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Date:
October 1948
Creator:
Lange, G.
Partner:
UNT Libraries Government Documents Department