Tytuł pozycji:
Holistic Low-Effort Model for Damage Tolerance Analysis in Preliminary Design
The paper presents reduced order results for three different realistic scenarios with respect to the damage tolerance behaviour. The scenarios are dedicated to stiffened structures and feature the fuselage side panel, the upper fuselage panel and a lower wing panel. A wide range of parameter variations is discussed and the influence on the inspection interval is shown. Results may be used both in preliminary aircraft design and structural optimisation.
1. The authors thankfully acknowledge the funding of the work presented here in the IMeLa project within the German Luftfahrtforschungsprogramm under project number 20A1709D. The computations were performed with resources provided by the North-German Supercomputing Alliance (HLRN).
2. Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023).
