Computational Aeroelastic Simulation of Rapidly Morphing Air Vehicles-Reference-Cited by-同舟云学术

Computational Aeroelastic Simulation of Rapidly Morphing Air Vehicles

Published:2010-04-12 Issue: Volume: Page:
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Container-title:51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th
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Author:

Selitrennik Evgeny,Karpel Moti,Levy Yuval

Publisher

American Institute of Aeronautics and Astronautics

Reference26 articles.

1. 2Gregory W. Reich, Jason C. Bowman, Brian Sanders, and Geoffrey J. Frank. "Development of an Integrated Multibody Morphing Simulation Tool", Inproceedings of 47thAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport,RhodeIland, May2006. AIAApaper2006-1892.

2. 3John N. Scarlett, Robert N. Canfield and Brian Sanders. "Multibody Dynamic Aeroelastic Simulation of a Folding Wing Aircraft", Inproceedings of 47thAIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, Newport, RhodeIland, May2006. AIAApaper2006-2135.

3. Coupling of substructures for dynamic analyses.

4. 5N. Ameri, M. H. Lowenberg and M.I. Friswell. "Modelling the Dynamic Response of a Morphing Wing with Active Winglets", Inproceedings of AIAA Atmospheric Flight Mechanics Conference and Exhibit, Hilton Head, South Carolina,August2007. AIAApaper 2007-6500.

5. 6B. Obradovic and K. Subbarao. "Modeling and Simulation to Study Flight Dynamics of a Morphable Wing Aircraft", Inproceedings of AIAA Modeling and Simulation Technologies Conference, Chicago, Illinois, August 2009. AIAApaper 2009-6240.

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3. Two-level Conceptual Design of Morphing Wings;54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2013-04-05

4. Prediction of transient responses of a folding wing during the morphing process;Aerospace Science and Technology;2013-01

5. Parameterized aeroelastic modeling and flutter analysis for a folding wing;Journal of Sound and Vibration;2012-01