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Wake dynamics and rotor-fuselage aerodynamic interactions

Kenyon, A.R. and Brown, R.E. (2009) Wake dynamics and rotor-fuselage aerodynamic interactions. Journal of the American Helicopter Society, 54 (1). 12003-1-12003-18. ISSN 0002-8711

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    Abstract

    The unsteady loads experienced by a helicopter are known to be strongly influenced by aerodynamic interactions between the rotor and fuselage; these unsteady loads can lead to deficiencies in handling qualities and unacceptable vibratory characteristics of the rotorcraft. This work uses a vorticity-based computational model to study the governing processes that underpin this aerodynamic interaction and aims to provide greater understanding of the wake dynamics in the presence of a fuselage, as well as an appreciation of how the geometry of the wake affects the loading on the fuselage. The well-known experiments using NASA's ROBIN fuselage are used to assess the accuracy of the computations. Comparisons of calculations against results from smoke visualization experiments are used to demonstrate the ability of the model to reproduce accurately the geometry of the rotor wake, and comparisons with inflow data from the experiments show the method to capture well the velocity field near to the rotor. The fuselage model is able to predict accurately the unsteady fuselage loading that is induced by blade passage and also by the inviscid interaction between the main rotor wake and fuselage.

    Item type: Article
    ID code: 27487
    Notes: ~Impact Factor 0.254, Half-Life >10.0
    Keywords: aerodynamic interactions, rotor and fuselage, unsteady loads, vibratory characteristics, vorticity-based computational model, aerodynamic interaction, rotor wake, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics
    Subjects: Technology > Mechanical engineering and machinery
    Technology > Motor vehicles. Aeronautics. Astronautics
    Department: Faculty of Engineering > Mechanical and Aerospace Engineering
    Related URLs:
      Depositing user: Ms Katrina May
      Date Deposited: 23 Sep 2010 09:56
      Last modified: 26 Nov 2012 05:46
      URI: http://strathprints.strath.ac.uk/id/eprint/27487

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