This paper gives a survey of Airbus' strategy about the low noise high-lift design. The different airframe noise sources on a commercial aeroplane are discussed. It will be completed by a physical description of especially those noise sources which typically occur on wings with deployed high-lift devices. Moreover the paper presents the concept to embed the noise criteria basically in the multidisciplinary high-lift design of Airbus. Finally, experimental techniques as well as theoretical tools suitable to describe the process of noise source generation and the identification of low-noise design parameters will be discussed.


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    Title :

    The Noise Criteria within Multidisciplinary High-Lift Design


    Contributors:
    Fischer, M. (author) / Bieler, H. (author) / Emunds, R. (author)


    Publication date :

    2006


    Size :

    9 Seiten





    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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