Aeroservoelastic Test of the Subsonic Ultra-Green Aircraft Research Truss-Braced Wing Model
Author:
Affiliation:
1. Boeing Research & Technology, St. Louis, Missouri 63042
2. Analytical Services & Materials Inc., Hampton, Virginia 23681
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/10.2514/1.G000265
Reference26 articles.
1. BradleyM.DroneyC. “Subsonic Ultra Green Aircraft Research: Phase I Final Report,” NASA CR-2011-216847, April 2011.
2. SUGAR Truss Braced Wing Full Scale Aeroelastic Analysis and Dynamically Scaled Wind Tunnel Model Development
3. BradleyM.DroneyC.AllenT. “Subsonic Ultra Green Aircraft Research: Phase II Final Report,” Contractor Rept. NNL08AA16B, May 2014.
4. Integrated Aeroservoelastic Optimization: Status and Direction
5. Aeroservoelastic Interaction Between Aircraft Structural and Control Design Schemes
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