Multi-Objective Multidisciplinary Optimization of Long-Endurance UAV Wing Using Surrogate Model in ModelCenter-Reference-Cited by-同舟云学术

Multi-Objective Multidisciplinary Optimization of Long-Endurance UAV Wing Using Surrogate Model in ModelCenter

Published:2008-06-14 Issue: Volume: Page:
ISSN:
Container-title:12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
language:
Short-container-title:

Author:

Long Teng¹,Liu Li¹,Zhou Sida¹,Wang Jiabo¹,Meng Lingtao¹

Affiliation:

1. Beijing Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-5918

Reference36 articles.

1. AIAA Multidisciplinary Design Optimization Technical Committee. "Current State of the Art on Multidisciplinary Design Optimization (MDO)", An AIAA White Paper. AIAA1991.

2. Sobieszczanski-Sobieski, J Haftka, R. T. "Multidisciplinary Aerospace Design Optimization: SurveyofRecent Developments",AIAA-96-0711,1996.

3. Giesing,J.P.Barthelemy,J. M. "ASummary of Industry MDOApplicationsandNeeds",AIAA1998.

4. Framework requirements for MDO application development

5. Padula, S. L., Gillian, R. E."Multidisciplinary Environments: A History of Engineering Framework Development",AIAA2006-7083,2006.

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. Aerostructural Wing Optimization Using a Structural Surrogate in a Coupled Adjoint Formulation;AIAA Journal;2024-05-21

2. A Comprehensive Design Method for Load, Stiffness, and Strength of High Altitude Long Endurance UAV;Lecture Notes in Electrical Engineering;2024

3. Design, experiments and multidisciplinary optimization of 2 degrees-of-freedom electromagnetic actuator for application in space vibration isolation;Advances in Mechanical Engineering;2017-12

4. Multidisciplinary Design and Optimization (MDO) Methodology for the Aircraft Conceptual Design;50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition;2012-01-09

5. Robust Multi-Objective Wing Design Optimization Via CFD Approximation Model;Engineering Applications of Computational Fluid Mechanics;2011-01