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Materialermüdung
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Eine 5-t-Zug-Druck-Dauerpruefmaschine der DVL
Statistical Analysis of the Time and Fatigue Strength of Aircraft Wing Structures
The fatigue strengths of some wrought aluminum alloys
Progress Report on Fatigue of Spot-welded Aluminum
Mechanical Tests of Macerated Phenolic Molding Material
Fatigue Characteristics of Spot-welded 24S-T Aluminum Alloy
Early Detection of Cracks Resulting from Fatigue Stressing
Axial Fatigue of 10 Airplane Wing-beam Specimens by the Resonance Method
Effect of Fatigue-stressing Short of Failure on Some Typical Aircraft Metals
Fatigue Tests on 1/8-inch Aluminum Alloy Rivets
An analysis of the fatigue life of an airplane wing structure under overload conditions
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
Biaxial Fatigue Strength of 24S-T Aluminum Alloy
Fatigue testing machine for applying a sequence of loads of two amplitudes
Static and fatigue strengths of high-strength aluminum-alloy bolted joints
Fatigue -- What it is and some ways of reducing its incidence
Fatigue -- What it is and some ways of reducing its incidence
Fatigue -- What it is and some ways of reducing its incidence
Review of fatigue of materials field
Elevated Temperature Fatigue Properties of Sae 4340 Steel
Investigation of the Structural Damping of a Full-scale Airplane Wing
Application of Boundary Layer Control to Helicopter Rotor Blades
Stress-life relation of the rolling-contact fatigue spin rig
STEEL SHEET AND STRIP 5Cr - 1.3Mo - 0.5V (0.38 - 0.43C)
Evaluation of the Sperry ASE Installed in the H-37 Helicopter
Astronautics Hydraulic Servo Cylinder 'Moog' 'D' Series, Vibration Testing and Life Testing
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
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