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Materialermüdung
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Thermal Stability of Residual Stresses in Differently Deep Rolled Surface Layers of Steel SAE 1045
Fatigue Instantaneous Self-Assessment (F-ISA): Development of a Short Mental Fatigue Rating
Implementing a Sleep Health Education and Sleep Disorders Screening Program in Fire Departments
Validation of Fatigue Modeling Predictions in Aviation Operations
Overview of Fatigue and Damage Tolerance Performance of SLM Alloy 718
Validating and Verifying Biomathematical Models of Human Fatigue
Rolling-element fatigue life of SAE 52100 steel hollow balls
Some factors affecting fatigue of aircraft structures
The development of performance tasks producing fatigue in man and other primates
FATIGUE OF METALS. II - CRACK PROPAGATION AND FINAL FAILURE
A simple environmental chamber for rotating- beam fatigue testing machines.
HIGHLY UNDEREXPANDED EXHAUST JETS AGAINST ADJACENT SURFACES
DESIGN CONCEPTS FOR MINIMUM WEIGHT, HIGH PERFORMANCE SUPERSONIC AIRCRAFT STRUCTURES
A SIMPLE ENVIRONMENTAL CHAMBER FOR R. R. MOORE FATIGUE TESTING MACHINES
VARIABLE-AMPLITUDE FATIGUE TESTS WITH PARTICULAR ATTENTION TO THE EFFECTS OF HIGH AND LOW LOADS
Stress-life relation of the rolling-contact fatigue spin rig
Preliminary metallographic studies of ball fatigue under rolling-contact conditions
Investigation of the Structural Damping of a Full-scale Airplane Wing
Fatigue testing machine for applying a sequence of loads of two amplitudes
Static and fatigue strengths of high-strength aluminum-alloy bolted joints
Biaxial Fatigue Strength of 24S-T Aluminum Alloy
Dislocation Theory of the Fatigue of Metals
Mechanical Properties of Five Laminated Plastics
Tensile, Fatigue, and Creep Properties of Forged Aluminum Alloys at Temperatures up to 800 F
An analysis of the fatigue life of an airplane wing structure under overload conditions
Effect of Fatigue-stressing Short of Failure on Some Typical Aircraft Metals
Fatigue Tests on 1/8-inch Aluminum Alloy Rivets
Early Detection of Cracks Resulting from Fatigue Stressing
Axial Fatigue of 10 Airplane Wing-beam Specimens by the Resonance Method
Progress Report on Fatigue of Spot-welded Aluminum