Overview
Engineering Services are provided based on profound expertise in Aeronautical Fatigue and Damage Tolerance. This includes specifically crack growth analyses using AFGROW and the development of Stress Intensity Factor (SIF) solutions with the support of ANSYS. Crack initiation analysis based on the Neuber notch methodology using CRINITY as part of the HSLU developed Structural Integrity Tool Box, see weblink below. Load spectrum development. Test plans from coupon to full scale testing and evaluation of test results. Failure investigations. Maintenance plans (MSG-3). Probabilty of detection (POD) studies for NDI.
Compliance Verification for Part 23 Aircraft.
