Experimental and analytical investigation of a monocoque wing model loaded in bending (1939)
NASA Technical Reports Server (NTRS) · leaf 36
(c) Loading by transverse forces figure 3.- Dimensions of the longi- at the spars. tudinal stiffeners on the Figure 1. Statement of the problem, compression skin. Wedges Loading beam Longitudinal stiffener Plate Figure 5.- Loading of the compres- sion skin at the center. Loading beam
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
