Experimental Studies of the Effective Width of Buckled Sheets (1936)
NASA Technical Reports Server (NTRS) · leaf 25
N.A.C.A. Technical Memorandum No. 814 Figs. 2,3,4 1 Figure 3.- Theoretical values 0.5 1 of buckling load of sheet; s = sheet thickness, v cr E = Young's modulus, t = spacing of edge stiffeners. Figure 2.- Factor k versus amount of exceeded buckling load. … Figure 4.- Experimentally defined curves for computing the effective width v/ith regards to the load taken up by the sheet (2 ^ to be written in equation (l) ) and with regards to the width of the sheet strip to be considered in the calculation of the "buckling load of the angle section {2*ty~ to…
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