Multi-Objective Design Optimization Framework for Conceptual Design of Families of Aircraft-Reference-Cited by-同舟云学术

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Multi-Objective Design Optimization Framework for Conceptual Design of Families of Aircraft

Published:2006-01-09 Issue: Volume: Page:
ISSN:
Container-title:44th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Versiani Cabral Leonardo¹,Paglione Pedro¹,Silva de Mattos Bento²

Affiliation:

1. Technological Institute of Aeronautics

2. Empresa Brasiliera de Aeronáutica S.A.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-1328

Reference4 articles.

1. J. Roskam, AirplaneDesign, PartV - Component Weight Estimation.S.L.: DAR Corporation,1999.

2. E. Torenbeek, Synthesis ofSubsonicAirplaneDesign.S.L.: Kluwer AcademicPublishers,1982.

Cited by 4 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. Multidisciplinary and Multi-Objective Optimization Considering Aircraft Program Cost and Airline Network;Journal of Air Transportation;2021-01

2. An Innovative Approach for integrated Airline Network and Aircraft Family Optimization;AIAA Aviation 2019 Forum;2019-06-14

3. Integrated Sizing and Optimization of Aircraft and Subsystem Architectures in Early Design;Journal of Aircraft;2018-09

4. Integrated Sizing and Multi-objective Optimization of Aircraft and Subsystem Architectures in Early Design;17th AIAA Aviation Technology, Integration, and Operations Conference;2017-06-05

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