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Volume 91 - February 1987

Contents

Page 4 of 6

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Front matter

  • AER volume 91 issue 903 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
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Front matter

  • AER volume 91 issue 906 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
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Inviscid theory of two-dimensional aerofoil/spoiler configurations at low speed

  • Part VI: The rapid deployment of a spoiler on a two-dimensional aerofoil

  • Published online by Cambridge University Press:
    04 July 2016, pp. 492-498

  • A method based on the shedding and convecting of discrete vortices has been developed to calculate the transient loading on an aerofoil-spoiler configuration when the spoiler is suddenly deployed to a particular angle. An innovation in the method is the introduction of Kutta conditions at the separation points.

    Although the variation of CL with time is highly irregular, qualitative trends can be deduced. For a range of aerofoil angle of incidence and spoiler angle deployment adverse lift effects (ie, when the lift initially increases) have been obtained, similar adverse lift effects have been measured in experiments.

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Front matter

  • AER volume 91 issue 905 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
    • Article
      • You have access
    • PDF
    • Export citation

Reviews

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Back matter

  • AER volume 91 issue 906 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. b1-b6
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  • AER volume 91 issue 903 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. b1-b2
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Front matter

  • AER volume 91 issue 902 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
    • Article
      • You have access
    • PDF
    • Export citation

Other

Page 4 of 6