Nonlinear Aeroelasticity of Highly Flexible Joined-Wing Aircraft using Unsteady Vortex-Lattice Method-Reference-Cited by-同舟云学术

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Nonlinear Aeroelasticity of Highly Flexible Joined-Wing Aircraft using Unsteady Vortex-Lattice Method

Published:2017-01-05 Issue: Volume: Page:
ISSN:
Container-title:58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
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Author:

Su Weihua¹,Huang Yanxin¹,Hammerton Jared R.¹

Affiliation:

1. University of Alabama, Tuscaloosa

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2017-1353

Reference37 articles.

1. The joined wing - An overview

2. Aeroelasticity of joined-wing airplane configurations - Past work and future challenges - a survey

3. Joined Wing Sensorcraft Aeroservoelastic Wind Tunnel Test Program

4. Nonlinear Aeroelasticity and Flight Dynamics of High-Altitude Long-Endurance Aircraft

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. Dynamic instability analysis of aeroelastic systems with application to aircraft wings;Physics of Fluids;2021-09

2. Structural and Aerodynamic Models for Aeroelastic Analysis of Corrugated Morphing Wings;AIAA Scitech 2020 Forum;2020-01-05

3. Correlation Studies of Geometrically Nonlinear Aeroelastic Formulations with Beam and Shell Elements;AIAA Scitech 2020 Forum;2020-01-05

4. Linearization and Analytical Aerodynamic Sensitivity of Unsteady Vortex-Lattice Aerodynamics;AIAA Scitech 2019 Forum;2019-01-06

5. Nonlinear Aeroelasticity of Morphing Wings with Corrugated Structures;AIAA Scitech 2019 Forum;2019-01-06

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