Existing interior noise reduction techniques for aircraft fuselages perform reasonably well at higher frequencies, but are inadequate at lower, particularly with respect to the low blade passage harmonics with high forcing levels found in propeller aircraft. A method is being studied which considers aircraft fuselages lines with panels alternately tuned to frequencies above and below the frequency to be attenuated. Adjacent panels would oscillate at equal amplitude, to give equal source strength, but with opposite phase. Provided these adjacent panels are acoustically compact, the resulting cancellation causes the interior acoustic modes to become cut off and therefore be non-propagating and evanescent. This interior noise reduction method, called Alternate Resonance Tuning (ART), is currently being investigated both theoretically and experimentally. This new concept has potential application to reducing interior noise due to the propellers in advanced turboprop aircraft as well as for existing aircraft configurations. This program summarizes the work carried out at Duke University during the third semester of a contract supported by the Structural Acoustics Branch at NASA Langley Research Center.


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    Titel :

    Aircraft interior noise reduction by alternate resonance tuning


    Beteiligte:

    Erscheinungsdatum :

    01.01.1989


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Aircraft Interior Noise Reduction by Alternate Resonance Tuning

    D. B. Bliss / J. A. Gottwald / R. Srinivasan et al. | NTIS | 1990


    Aircraft interior noise reduction by alternate resonance tuning

    Bliss, Donald B. / Gottwald, James A. / Srinivasan, Ramakrishna et al. | NTRS | 1990


    Interior noise reduction by alternate resonance tuning

    Bliss, Donald B. / Gottwald, James A. / Bryce, Jeffrey W. | NTRS | 1987