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    Title :

    Acoustic Wind Tunnel Test with 18% Scale Half-span Model toward FQUROH Second Flight Demonstration (AIAA 2018-4086)



    Conference:

    Aeroacoustics (Conference)



    Publication date :

    2018-01-01


    Size :

    21 pages



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English



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    Further Noise Reduction Design for Landing Gear toward FQUROH Second Flight Demonstration (AIAA 2018-3300)

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    Nr. 4086

    DataCite | 1923