Stress intensity factors in lugs (through-thickness cracks).
Abstract:ESDU 81029 provides values of the geometrical factor in the stress intensity factor for round-ended lugs loaded axially by a single central clearance-fit pin. The cracks are assumed to be a uniform depth through the full thickness of the lug. Values are provided for single cracks on one side of the pin or two cracks of equal length on opposite sides of the pin. The data are provided both graphically and in tabular form. The latter are such that linear interpolation between adjacent values provides sufficient accuracy for crack growth calculations.
|Data Item ESDU 81029|
- Aircraft Noise
- Fatigue - Endurance Data
- Fatigue - Fracture Mechanics
- Fluid Mechanics, Internal Flow
- Fluid Mechanics, Internal Flow (Aerospace)
- Heat Transfer
- Physical Data, Chemical Engineering
- Stress and Strength
- Transonic Aerodynamics
- Vibration and Acoustic Fatigue
- Wind Engineering
Aerospace Materials Data
Additional Engineering References