Test results discussed with reference to present knowledge of fatigue of materials and joints used in aircraft construction.
Fatigue strength and related characteristics of aircraft joints -- II -- Fatigue characteristics of sheet and riveted joints of 0.040-inch 24S-T, 75S-T, and R303- T275 aluminum alloys
Nat Advisory Committee Aeronautics -- Tech Note
1948
97 pages
Bibliography
Aufsatz (Zeitschrift)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
The Fatigue Strength of Riveted Joints
Emerald Group Publishing | 1957
|Fatigue strength of riveted joints and lugs
Engineering Index Backfile | 1956
|