Investigation of methods for including real vane geometry in predictions of fan broadband noise

Sheryl M. Grace, Dorien Villafranco, Andy Wixom

    Research output: Chapter in Book/Report/Conference proceedingConference contribution

    1 Scopus citations

    Abstract

    Two methods for increasing the geometric fidelity of a fan-stage, broadband, interaction-noise model are investigated. The increase in fidelity is sought in order to eliminate the dependence on stagger selection that exists when vanes are modeled as flat plates. First, a blade-vortex interaction (BVI) technique is considered for obtaining a subsonic, 2D, unsteady, real-geometry cascade response that can be readily incorporated into an existing low-order broadband model. A description of the overall method and results from the development of the cascade-BVI are presented. Second, a method for utilizing a linearized Euler calculation that has been presented in the literature previously is reviewed and discussed. Preliminary findings from an attempt to utilize LINFLUX as the linearized Euler solver in the broadband model are described.

    Original languageEnglish (US)
    Title of host publication22nd AIAA/CEAS Aeroacoustics Conference
    PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
    ISBN (Print)9781624103865
    DOIs
    StatePublished - 2016
    Event22nd AIAA/CEAS Aeroacoustics Conference, 2016 - Lyon, France
    Duration: May 30 2016Jun 1 2016

    Publication series

    Name22nd AIAA/CEAS Aeroacoustics Conference, 2016

    Other

    Other22nd AIAA/CEAS Aeroacoustics Conference, 2016
    Country/TerritoryFrance
    CityLyon
    Period5/30/166/1/16

    All Science Journal Classification (ASJC) codes

    • Electrical and Electronic Engineering
    • Aerospace Engineering

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