The Active Aeroelastic Wing Flight Research Program - Technical program and model analytical development

Author:

Pendleton Ed1,Bessette Denis2,Field Pete3,Miller Gerry4,Griffin Kenneth5

Affiliation:

1. USAF, Air Vehicles Directorate, Wright-Patterson AFB, OH

2. NASA, Flight Research Center, Edwards AFB, CA

3. Boeing-Phantom Works, Saint Louis, MO

4. Boeing-Phantom Works, Seal Beach, CA

5. Southwest Research Inst., San Antonio, TX

Publisher

American Institute of Aeronautics and Astronautics

Reference16 articles.

1. Miller, G.D."AnActiveFlexibleWing Multi-Disciplinary Design Optimization Method," AIAA Paper No.94-4412-CP.

2. Summary of an Active Flexible Wing program

3. Application of Active Flexible Wing technology to the Agile Falcon

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1. A Study of the Active Aeroelastic Wing Concept for a Delta Wing Aircraft;AIAA Scitech 2021 Forum;2021-01-04

2. Investigation of Robust Combination Control for Elastic Vehicle Based on Reduced-Order Model;Applied Mechanics and Materials;2013-08

3. Study on gust alleviation control and wind tunnel test;Science China Technological Sciences;2013-01-18

4. Controllability Analysis of Flexible Variable Sweep Control Wing;Advanced Materials Research;2012-06

5. A Novel Mechanism for Wing Warping;49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference <br> 16th AIAA/ASME/AHS Adaptive Structures Conference<br> 10t;2008-04-07

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