Constructive design models for multidisciplinary optimization of fiber composite structures

Author:

ESCHENAUER H.1,SCHUHMACHER G.1,KRAMMER J.2

Affiliation:

1. Siegen Univ., Germany

2. MBB GmbH, Military Aircraft Div., Munich, Germany

Publisher

American Institute of Aeronautics and Astronautics

Reference25 articles.

1. Dissertation, TU Munchen, 1991.

2. Procedure SAPOP - A General Tool for Multicriteria

Cited by 5 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. Multi-disciplinary design optimization of composite structures: A review;Composite Structures;2022-01

2. Design Procedure for Optimum Fiber Composite Airframe Structures Within an Automated Multidisciplinary Design and Optimization Process;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2018

3. Multidisciplinary Wing Optimization Using a Wing Box Layout Concept and a Parametric Thickness Model;9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;2002-09-04

4. Multidisciplinary Design Optimization of a Regional Aircraft Wing Box;9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization;2002-09-04

5. Concurrent engineering in design of aircraft structures;Journal of Aircraft;1995-03

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