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- W117603923 abstract "ABSTRACT This paper documents an invited presentation given to The Boeing Company, Seattle,Washington on September 9, 1997. The audience consisted of structural dynamic and flight testengineers from the Boeing Commercial Airplane Group who were interested in discussingresearch which may be applied to future flight flutter test programs. A method to compute robustflutter margins is described which is a significant departure from traditional methods. Thismethod uses the structured singular value, _t, to compute a flutter margin which directly accountsfor modeling errors such that a worst-case flutter margin is computed with respect to thoseerrors. This method may be applied in several ways. A post-flight application uses data sets frommultiple test points to compute worst-case flutter margins and a worst-case flight envelope. Anon-line implementation computes flutter margins at each test point to track the flutter marginsduring a flight test. This on-line implementation is the basis for a flutterometer flight test toolthat displays the distance to flutter at a given test point. Such a tool was not previously possibleusing traditional flutter flight test analysis methods. The F/A-18 System Research Aircraft wasused to demonstrate these applications using flight data recorded from test points throughout theflight envelope.NOMENCLATURECKMPPQ" @default.
- W117603923 created "2016-06-24" @default.
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- W117603923 date "1997-10-01" @default.
- W117603923 modified "2023-09-25" @default.
- W117603923 title "A Presentation on Robust Flutter Margin Analysis and a Flutterometer" @default.
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