Application of MDO Techniques to the Preliminary Design of Morphed Aircraft-Reference-Cited by-同舟云学术

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Application of MDO Techniques to the Preliminary Design of Morphed Aircraft

Published:2006-09-06 Issue: Volume: Page:
ISSN:
Container-title:11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
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Author:

Ricci Sergio,Terraneo Mauro

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2006-7018

Reference17 articles.

1. 1Crowe, C. and Sater, J. “Smart Aircraft Structures,” AGARD Paper, 1997.

2. 3Bowman, J., Sanders, B., andWeisshaar, T. “EvaluatingtheImpactofMorphingTechnologiesonAircraftPerformance,” 43th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference, 22-25 April, Denver, Colorado, USA, April 2002.

3. Integrated Servostructural Optimization in the Design of Aerospace Systems

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. On the use of geometry design variables in the MDO analysis of wing structures with aeroelastic constraints on stability and response;Aerospace Science and Technology;2011-04

2. A Two Levels Approach for the Optimal Design of Morphing Airfoils;13th AIAA/ISSMO Multidisciplinary Analysis Optimization Conference;2010-06-26

3. Designing a family of reconfigurable vehicles using multilevel multidisciplinary design optimization;Structural and Multidisciplinary Optimization;2008-10-22

4. Design and Optimization of Reconfigurable Vehicle Platforms;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

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