Investigation of local load introduction methods in aircraft pre-design-Reference-Cited by-同舟云学术

Investigation of local load introduction methods in aircraft pre-design

Published:2012-09 Issue:1 Volume:21 Page:31-40
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Hürlimann F.,Kelm R.,Dugas M.,Kress G.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference10 articles.

1. C. Anhalt, H.P. Monner, E. Breitbach, Interdisciplinary wing design – structural aspects, German Aerospace Center (DLR), 2003.

2. S.R.H. Dean, J.J. Doherty, T.R. Wallace, Impact of Fuel Systems on Aircraft Design Using a MDO Process, Aerospace Consulting, QinetiQ, Farnborough, UK, 2009.

3. Ein Beitrag zur Auslegung von Faserverbundtragflügeln im Vorentwurf, Institut für Flugzeugbau;Dugas,2002

4. C. Hanske, E. Kropp, TN-ESGD-03/2001 (SMT loads), Internal Report, Airbus Deutschland GmbH, 2001.

5. Mass estimation of transport aircraft wingbox structures with a CAD/CAE-based multidisciplinary process;Huerlimann;Aerospace Science & Technology,2011

Cited by 15 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Natural laminar flow leading edge: Requirements, design, and experimental validation under operational loads;Aerospace Science and Technology;2024-03

2. Modeling, analysis and validation of the structural response of a large-scale composite wing by ground testing;Composite Structures;2023-05

3. Management and intelligent control of in‐flight fuel distribution in a commercial aircraft;Expert Systems;2022-06-18

4. Identification of the key design inputs for the FEM-based preliminary sizing and mass estimation of a civil aircraft wing box structure;Aerospace Science and Technology;2022-02

5. Correlation of CFRP and AA7075 Aircraft Wing box structure using FEM;IOP Conference Series: Materials Science and Engineering;2021-03-01