Inside Out Library · ExploreWrinkling Phenomena of Thin Flat Plates Subjected to Shear Stresses (1931)NASA Technical Reports Server (NTRS) · leaf 43N.A.C.A. Technical Memorandum No.601 Figs.25,26- Fig.25 Wrinkling by, s = 4.83 kg/cm,edge loading.NASA Technical Reports Server (NTRS)Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.More pictures from Wrinkling Phenomena of Thin Flat Plates Subjected to Shear StressesMore like this