Fatigue strength and related characteristics of aircraft joints. : 2 - Fatigue characteristics of sheet and riveted joints of 0.040-inch 24S-T, 75S-T, and R303-T275 aluminum alloys / H.W. Russell [and others]

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Bibliographic Details
Main Author:	Russell, H. W.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1485.
Subjects:	Aluminum alloys > Fatigue. Riveted joints > Testing. Strains and stresses.

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Call Number:	Y 3.N 21/5:6/1485
Y 3.N 21/5:6/1485	Available Place a Hold