Summary
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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© 2006 Springer-Verlag Berlin Heidelberg
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Fischer, M., Bieler, H., Emunds, R. (2006). The Noise Criteria within Multidisciplinary High-Lift Design. In: Rath, HJ., Holze, C., Heinemann, HJ., Henke, R., Hönlinger, H. (eds) New Results in Numerical and Experimental Fluid Mechanics V. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 92. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-33287-9_43
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DOI: https://doi.org/10.1007/978-3-540-33287-9_43
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-33286-2
Online ISBN: 978-3-540-33287-9
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