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Interactional aerodynamics and acoustics of a hingeless coaxial helicopter with an auxiliary propeller in forward flight

Kim, Hyo Wan and Kenyon, Adam R. and Duraisamy, Karthikeyan and Brown, Richard (2009) Interactional aerodynamics and acoustics of a hingeless coaxial helicopter with an auxiliary propeller in forward flight. Aeronautical Journal, 113 (1140). pp. 65-78. ISSN 0001-9240

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    Abstract

    The aerodynamics and acoustics of a generic coaxial helicopter with a stiff main rotor system and a tail-mounted propulsor are investigated using Brown's Vorticity Transport Model. In particular, the model is used to capture the aerodynamic interactions that arise between the various components of the configuration. By comparing the aerodynamics of the full configuration of the helicopter to the aerodynamics of various combinations of its sub-components, the influence of these aerodynamic interactions on the behaviour of the system can be isolated. Many of the interactions follow a simple relationship between cause and effect. For instance, ingestion of the main rotor wake produces a direct effect on the unsteadiness in the thrust produced by the propulsor. The causal relationship for other interdependencies within the system is found to be more obscure. For instance, a dependence of the acoustic signature of the aircraft on the tailplane design originates in the changes in loading on the main rotor that arise from the requirement to trim the load on the tailplane that is induced by its interaction with the main rotor wake. The traditional approach to the analysis of interactional effects on the performance of the helicopter relies on characterising the system in terms of a network of possible interactions between the separate components of its configuration. This approach, although conceptually appealing, may obscure the closed-loop nature of some of the aerodynamic interactions within the helicopter system. It is suggested that modern numerical simulation techniques may be ready to supplant any overt reliance on this reductionist type approach and hence may help to forestall future repetition of the long history of unforseen, interaction-induced dynamic problems that have arisen in various new helicopter designs.

    Item type: Article
    ID code: 27535
    Notes: Also presented at 9th International Powered Lift Conference, IPLC2008. This is a variant record V: 27544
    Keywords: aerodynamic interactions, acoustics, coaxial helicopter, vorticity transport model, rotor wake, numerical simulation techniques, helicopter design, Mechanical engineering and machinery, Motor vehicles. Aeronautics. Astronautics, Mechanical Engineering, Aerospace Engineering, Computational Mechanics, Modelling and Simulation
    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: 29 Sep 2010 12:39
    Last modified: 04 Jun 2014 03:00
    URI: http://strathprints.strath.ac.uk/id/eprint/27535

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