Description
Recent studies of the occurrence of post-flutter limit cycle oscillations (LCO) of the F-16 have provided good support to the long-standing hypothesis that this phenomenon involves a nonlinear structural damping.
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Contributors
- Song, Pengchao (Author)
- Mignolet, Marc P (Thesis advisor)
- Chattopadhyay, Aditi (Committee member)
- Oswald, Jay (Committee member)
- Arizona State University (Publisher)
Date Created
The date the item was original created (prior to any relationship with the ASU Digital Repositories.)
2015
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Note
- Partial requirement for: M.S., Arizona State University, 2015Note typethesis
- Includes bibliographical references (pages 69-71)Note typebibliography
- Field of study: Mechanical engineering
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by Pengchao Song