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- W311370829 abstract "Abstract : A method is set forth for predicting the acoustically induced structural vibration in transport category aircraft. Charts are presented which correlate third-octave random noise and vibration levels at various confidence levels, for the frequency range of 50 to 2500 Hertz. The prediction charts are based on measured data from modern transport aircraft and are presented for the normal direction, ground operation, and a reference structural mass and rigidity. Shell-type structure (fuselage, pods, fairings) and box-type structure (wing, horizontal/vertical stabilizer) are treated separately. Means are provided for predicting lateral and tangential vibration, vibration in pressurized cruise flight, and for correcting for changes in structural mass and rigidity. Application of the method to a hypothetical airplane design case is illustrated in an example." @default.
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- W311370829 date "1974-09-01" @default.
- W311370829 modified "2023-09-28" @default.
- W311370829 title "A Method for Predicting Acoustically Induced Vibration in Transport Aircraft" @default.
- W311370829 doi "https://doi.org/10.21236/ada004215" @default.
- W311370829 hasPublicationYear "1974" @default.
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