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    Adapting a propeller noise model for aircraft at cruising altitudes

    Access Status
    Fulltext not available
    Authors
    Blunt, D.
    Jones, Adrian
    Mewett, D.
    Date
    2014
    Type
    Conference Paper
    
    Metadata
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    Citation
    Blunt, D. and Jones, A. and Mewett, D. 2014. Adapting a propeller noise model for aircraft at cruising altitudes.
    Source Title
    INTERNOISE 2014 - 43rd International Congress on Noise Control Engineering: Improving the World Through Noise Control
    ISBN
    9780909882037
    School
    Centre for Marine Science and Technology
    URI
    http://hdl.handle.net/20.500.11937/52806
    Collection
    • Curtin Research Publications
    Abstract

    An existing propeller harmonic noise model is adapted to incorporate the effects of a stratified atmosphere so that predictions can be made of the ground-level noise for an aircraft flying at cruising altitudes. Specifically, the speed of sound and the atmospheric absorption are both made functions of altitude. The effects of refraction and ground reflection are examined, but deemed small enough to exclude from the initial model adaptation. The adapted model is applied to long-range acoustic data for a turboprop aircraft at three different cruising altitudes. The results show that a relatively good fit can be found between the model and the experimental data at the Doppler-shifted blade passing frequency within a range of source radiation angles from 30° to 110° with respect to the aircraft's direction of travel. The results also highlight the influence of molecular oxygen on the atmospheric absorption of the propeller harmonics. Recommendations are made for further improvements to the model.

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