Limit-Cycle Oscillation of the Subsonic Ultra-Green Aircraft Research Truss-Braced Wing Aeroelastic Model-Reference-Cited by-同舟云学术

Limit-Cycle Oscillation of the Subsonic Ultra-Green Aircraft Research Truss-Braced Wing Aeroelastic Model

Published:2017-09 Issue:5 Volume:54 Page:1605-1613
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Bartels Robert E.¹,Funk Christie J.¹,Scott Robert C.¹

Affiliation:

1. NASA Langley Research Center, Hampton, Virginia 23681

Funder

Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.C034064

Reference22 articles.

1. BradleyM. K.DroneyC. K.AllenT. J. “Subsonic Ultra Green Aircraft Research: Truss Braced Wing Aeroelastic Test Report,” NASA NNL08AA16B, Boeing Company, CR, June 2014.

2. Computed and Experimental Flutter/LCO Onset for the Boeing Truss-Braced Wing Wind Tunnel Model

3. SUGAR Truss Braced Wing Full Scale Aeroelastic Analysis and Dynamically Scaled Wind Tunnel Model Development

4. Aeroservoelastic Test of the Subsonic Ultra-Green Aircraft Research Truss-Braced Wing Model

5. Nonlinear Flutter Aspects of the Flexible HIgh-Speed Civil Transport Semispan Model

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