Cumulative damage in fatigue
- 1 January 1956
- book chapter
- Published by Springer Nature
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- A Photoelastic-Fatigue Programme of Experimental Research in Connection with Bolted JointsJournal of the Royal Aeronautical Society, 1954
- The Estimation of Fatigue Damage in Aircraft Wing StructuresJournal of the Royal Aeronautical Society, 1954
- A Method for Determining the “Safe” Life of an Aircraft Wing From Fatigue Test ResultsJournal of the Royal Aeronautical Society, 1954
- Design Criterion for Fatigue of WingsJournal of the Royal Aeronautical Society, 1953
- Fatigue Life of Wing Components for Civil AircraftJournal of the Royal Aeronautical Society, 1952
- Strength of Aeroplanes in Relation to Repeated LoadsAeronautical Quarterly, 1950
- The Behaviour of Structures Under Repeated LoadsJournal of the Royal Aeronautical Society, 1947
- Cumulative Damage in FatigueJournal of Applied Mechanics, 1945
- Discussion: “Fatigue Failure From Stress Cycles of Varying Amplitude” (Langer, B. F., 1937, ASME J. Appl. Mech., 4, pp. A160–A162)Journal of Applied Mechanics, 1938
- Discussion: “Fatigue Failure From Stress Cycles of Varying Amplitude” (Langer, B. F., 1937, ASME J. Appl. Mech., 4, pp. A160–A162)Journal of Applied Mechanics, 1938