Fluid-Structure Interaction of HALE Wing Configuration with an Efficient Moving Grid Method-Reference-Cited by-同舟云学术

Fluid-Structure Interaction of HALE Wing Configuration with an Efficient Moving Grid Method

Published:2008-01-07 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA Aerospace Sciences Meeting and Exhibit
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Author:

Carnie Greg¹,Qin Ning¹

Affiliation:

1. Department of Mechanical Engineering, University of Sheffield

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2008-309

Reference44 articles.

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2. Heliplat®: high altitude very-long endurance solar powered UAV for telecommunication and Earth observation applications

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4. F. Liu, J. Cai, Y. Zhu, H. M. Tsai, A. S. F. Wong. Calculation of wing flutter by a coupled fluid-structure method.JournalofAircraftVol.38,No.2,March-April2001.

5. E. Lee-Rausch and J. T. Batina. Calculation of Agard Wing 445.6 flutter using Navier-Stokes aerodynamics AIAApaper93-3476,1993.

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