Robust Flutter Suppression and Wind-Tunnel Tests of a Three-Dimensional Wing-Reference-Cited by-同舟云学术

Robust Flutter Suppression and Wind-Tunnel Tests of a Three-Dimensional Wing

Published:2018-11 Issue:6 Volume:31 Page:04018099
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Qian Wenmin¹^ORCID

Affiliation:

1. Engineer, Beijing Key Laboratory of Civil Aircraft Structures and Composite Materials, Beijing Aeronautical Science and Technology Research Institute of Commercial Aircraft Corporation of China, Future Science and Technology Park, Changping District, Beijing 102211, China. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000925

Reference34 articles.

1. Gain-Scheduled Linear Fractional Control for Active Flutter Suppression

2. Robust Aeroelastic Stability Analysis Considering Frequency-Domain Aerodynamic Uncertainty

3. Comparison of Adaptive Control Architectures for Flutter Suppression

4. Christhilf D. M. B. Moulin E. Ritz P. C. Chen K. M. Roughen and B. Perry. 2012. “Characteristics of control laws tested on the semi-span super-sonic transport (S4T) wind-tunnel model.” In Proc. 53rd AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conf. Reston VA: American Institute of Aeronautics and Astronautics.

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