Technical notes. 1485. Fatigue strength and related characteristic of aircraft Joints: 2. Fatigue characteristics of sheet and riveted joints of 0.040-inch 24S-T, 75S-T, and R30.1-T275 aluminum alloys [with list of references]: by H. W. Russell, L. R. Jackson, H. J. Grover, and W. W. Beaver.

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