ZEUS-DO: Design Oriented CFD-Based Unsteady Aerodynamics for Flight Vehicle Shape Optimization-Reference-Cited by-同舟云学术

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ZEUS-DO: Design Oriented CFD-Based Unsteady Aerodynamics for Flight Vehicle Shape Optimization

Published:2010-04-12 Issue: Volume: Page:
ISSN:
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:

Chen P.C.,Zhang Z,Livne Eli

Publisher

American Institute of Aeronautics and Astronautics

Reference23 articles.

1. Analytic Sensitivities and Approximations in Supersonic and Subsonic Wing/Control Surface Unsteady Aerodynamics

2. Unsteady-Aerodynamic Shape Sensitivities for Airplane Aeroservoelastic Configuration Optimization

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 Distributed Morphing Control of an Aeroelastic Wing for a Small Drone;Journal of Aircraft;2019-11

2. Design-Oriented Computational Fluid Dynamics-Based Unsteady Aerodynamics for Flight-Vehicle Aeroelastic Shape Optimization;AIAA Journal;2015-12

3. Integrated Aeroservoelastic Design Optimization of Actively Controlled Strain-Actuated Flight Vehicles;AIAA Journal;2014-06

4. Gust Response Parameter Optimization of Two-Dimensional Airfoil Section;Applied Mechanics and Materials;2013-07

5. Towards CFD Based Aeroservoelastic Flight Vehicle Shape Optimization - New Capabilities and New Results with ZEUS-DO;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

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