NASA Technical Note [NASA TN D-543]: Fatigue-crack propagation in aluminum-alloy tension panels - Washington. National Aeronautics and Space Administration (NASA); Whaley, Richard E.; Kurzhals, Peter R. (NASA Washington, 1960)
Bound together NASA TN D-541 to 550
Bound vol. Acc. No. 65466 contains Acc. No. TR15854 to TR15862
Keywords: Stresses and loades