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- W25990532 abstract "The dynamic aeroelastic instability of flutter is an important factor in the design of modern high-speed, flexible aircraft. The current trend is toward the creative use of composites to delay flutter. To obtain an optimum design, we need an accurate as well as efficient model. As a first step towards this goal, flutter analysis is carried out for an unswept composite box beam using a linear structural model and Theodorsen's unsteady aerodynamic theory. Structurally, the wing was modeled as a thin-walled box-beam of rectangular cross section. Theodorsen's theory was used to get 2-D unsteady aerodynamic forces, which were integrated over the span. A free-vibration analysis is carried out. These fundamental modes are used to get the flutter solution using the V-g method. Future work is intended to build on this foundation." @default.
- W25990532 created "2016-06-24" @default.
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- W25990532 date "1995-02-21" @default.
- W25990532 modified "2023-09-25" @default.
- W25990532 title "Flutter analysis of composite box beams" @default.
- W25990532 hasPublicationYear "1995" @default.
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