Integrated aeroservoelastic wing synthesis by nonlinear programming/approximation concepts
Author:
Affiliation:
1. University of Washington, Seattle, Washington 98195
2. University of California, Los Angeles, California 90024
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.20933
Reference67 articles.
1. Aeroservoelastic Encounters
2. Optimization of flexible wing structures subject to strength and induced drag constraints
Cited by 12 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. Integrated Aeroservoelastic Design Optimization of Actively-Controlled Strain-Actuated Flight Vehicles;46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference;2005-04-18
2. Integrated Design of Aerodynamics and Control System for Micro Air Vehicles.;JSME International Journal Series C;2000
3. Integrated Aeroservoelastic Optimization: Status and Direction;Journal of Aircraft;1999-01
4. Multidisciplinary aerospace design optimization: survey of recent developments;Structural Optimization;1997-08
5. Analytic Sensitivities and Approximations in Supersonic and Subsonic Wing/Control Surface Unsteady Aerodynamics;Journal of Aircraft;1997-05
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