Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration-Reference-Cited by-同舟云学术

Dynamic Nonlinear Aeroelastic Analysis of the Joined Wing Configuration

Published:2012-04-23 Issue: Volume: Page:
ISSN:
Container-title:53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA
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Author:

Bhasin Samarth,Chen Ping,Wang Zhicun,Demasi Luciano

Publisher

American Institute of Aeronautics and Astronautics

Reference44 articles.

1. The joined wing - An overview

2. Structural Weight Comparison of a Joined Wing and a Conventional Wing

3. 3Selberg, B. and Cronin, D. “Aerodynamic-Structural Optimization of Positive/Negative Stagger Joined Wing Configurations,” AIAA Paper 86-2626, AIAA/AHS/ASEE Aircraft Systems, Design and Technology Meeting, Dayton, Ohio.

4. 5Smith, S., Cliff, S., and Kroo, I. “The Design of a Joined Wing Flight Demonstrator Aircraft,” AIAA Paper 87-2930. AIAA/AHS/ASEE Aircraft Systems, Design and Technology Meeting, Saint Louis, MO.

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1. Post-flutter response of a flexible cantilever plate in low subsonic flows;International Journal of Non-Linear Mechanics;2017-05

2. Challenges, Ideas, and Innovations of Joined-Wing Configurations: A Concept from the Past, an Opportunity for the Future;Progress in Aerospace Sciences;2016-11

3. Phenomenology of Nonlinear Aeroelastic Responses of Highly Deformable Joined-wings Configurations;55th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2014-01-10