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- W1963480618 abstract "It is essential to determine eight conditions at which aeroelastic instabilities occur. Flight-test methods can be dangerous and costly, whereas analytical methods may not accurately predict the eutter boundary. An approach to computing eutter boundaries based on the structured singular value is presented. The aeroelastic system is formulated inarobust stabilityframework byparameterizingaround dynamicpressure and introducinguncertainty operators to account for modelingerrors. Flight data can be used tovalidate the robust systemmodel and increase accuracy of the eutter margin estimate. Flutter margins are generated for the F/A-18 Systems Research Aircraft using this method and traditional methods. Extensive e ight data from conditions throughout the eight envelope areanalyzed todeterminethelevelsof uncertaintyinatheoreticalmodel. Therobust marginsdemonstratethat the e ight conditions for e utter may lie closer to the eight envelope than previously estimated by traditional analysis." @default.
- W1963480618 created "2016-06-24" @default.
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- W1963480618 date "1997-05-01" @default.
- W1963480618 modified "2023-10-16" @default.
- W1963480618 title "Robust Flutter Margins of an F/A-18 Aircraft from Aeroelastic Flight Data" @default.
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- W1963480618 doi "https://doi.org/10.2514/2.4082" @default.
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