Nonlinear Aeroelastic Testing
Nonlinear Aeroelastic Testing is a systematic experimental methodology within aeroelasticity that characterizes the dynamic interaction between aerodynamic, elastic, and inertial forces in structural systems where nonlinearities—such as large deformations, material hysteresis, or flow separation—significantly influence the system's response, thereby distinguishing it from linearized approaches that assume proportionality and superposition.
7
Publications
355
Citations
24
Authors
12
Institutions
Publications per year
2017–2026
1
Parents
7
X-HALE: A Very Flexible UAV for Nonlinear Aeroelastic Tests
Carlos E. S. Cesnik, Patrick Senatore, Weihua Su et al. · 2010 · 27 citations
Engineering, Aerospace Engineering, Mechanical Engineering +17
1–5 of 7
24
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12
University of Michigan
Ann Arbor, United States
3 h-index
10 publications
508 citations
United States Air Force
Arlington, United States
2 h-index
2 publications
116 citations

U.S. Air Force Institute of Technology
Dayton, United States
1 h-index
1 publications
89 citations

University of Toronto
Toronto, Canada
1 h-index
2 publications
26 citations
Texas A&M University
College Station, United States
1 h-index
2 publications
262 citations
Massachusetts Institute of Technology
Cambridge, United States
1 h-index
2 publications
124 citations

United States Air Force Research Laboratory
Wright-Patterson AFB, United States
1 h-index
1 publications
27 citations
Lockheed Martin (Canada)
Ottawa, Canada
1 h-index
2 publications
22 citations
1–8 of 12
1 publications · 89 citations
1
h-index
1 publications · 22 citations
1
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1 publications · 131 citations
1
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1 publications · 62 citations
1
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1 publications · 13 citations
1
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