F-16 Limit-Cycle Oscillation Analysis Using Nonlinear Damping

Title
F-16 Limit-Cycle Oscillation Analysis Using Nonlinear Damping
Authors
Keywords
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Journal
JOURNAL OF AIRCRAFT
Volume 53, Issue 1, Pages 243-250
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Online
2015-07-27
DOI
10.2514/1.c033315

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