Holistic Low-Effort Model for Damage Tolerance Analysis in Preliminary Design-Reference-Cited by-同舟云学术

Holistic Low-Effort Model for Damage Tolerance Analysis in Preliminary Design

Published:2022-09-01 Issue:3 Volume:2022 Page:1-20
ISSN:2545-2835
Container-title:Transactions on Aerospace Research
language:en
Short-container-title:

Author:

Rohdenburg Michael¹^ORCID,Runge Fabian¹^ORCID,Haupt Matthias¹^ORCID,Markgraf Lennart²^ORCID,Horst Peter¹^ORCID,Heimbs Sebastian¹^ORCID

Affiliation:

1. Technische Universität Braunschweig, Institute of Aircraft Design and Lightweight Structures , Hermann-Blenk-Str. 35 , Braunschweig , Germany

2. IBK Innovation GmbH & Co. KG , Butendeichsweg 2 , Hamburg , Germany

Abstract

Abstract 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.

Publisher

Walter de Gruyter GmbH

Link

https://www.sciendo.com/pdf/10.2478/tar-2022-0013

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