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- W2006346094 abstract "flutter boundary is plotted for zero damping and for rj = 0.1 damping added to the nacelle strut in side bending. The addition of damping increases the bandwidth of nacelle side bending frequency in which the nacelle tuning suppresses flutter; the chimney becomes wider with the addition of damping. In addition, the flutter speed is increased with the addition of damping at some of the other nacelle side bending natural frequencies studied but not at all of them. Conclusion The addition of damping to the nacelle strut in this study improved the airplane flutter characteristics. This addition of damping to nacelle struts has become practical with the recent development of materials such as 3M's ISD 113. An application of these materials is documented on an F-15 application in Ref. 1. Their durability in a harsh environment has been demonstrated on the TF-30 inlet guide vane treatment discussed in Ref. 2. A large selection of damping materials is currently available for the designer to choose from." @default.
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- W2006346094 date "1980-07-01" @default.
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- W2006346094 title "Comment on Prediction of Performance of Low-Pressure-Ratio Thrust-Augmentor Ejectors" @default.
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- W2006346094 doi "https://doi.org/10.2514/3.57936" @default.
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