The random decrement technique applied to the YF-16 flight flutter tests
Author:
Affiliation:
1. General Dynamics Corp., Fort Worth, Tex.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1975-776
Reference5 articles.
1. YF16 active-control-system/structural dynamics interaction instability
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1. Wind-Tunnel Study of the Autoregressive Moving-Average Flutter Prediction Method;Journal of Aircraft;2019-07
2. Assessment of Advanced Flutter Flight-Test Techniques and Flutter Boundary Prediction Methods;Journal of Aircraft;2018-09
3. Wind-Tunnel Study of the ARMA Flutter Prediction Method;2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2018-01-07
4. Flutter Prediction Using Continuous Wavelet Transform;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2009
5. Estimation of flutter boundary from random responses due to turbulence at subcritical speeds;Journal of Aircraft;1981-10
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