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Volume 106 - January 2002

Contents

Page 5 of 6

Front matter

  • ARE Volume 106 issue 1066 Cover and Front matter

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

Front matter

  • AER volume 106 issue 1060 Cover and Front matter

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

Back matter

  • ARE Volume 106 issue 1066 Cover and Back matter

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

  • The effect of a sequence of cavities on boundary-layer separation at M = 8.2

  • Z. He, J. Xiong, C. Lebas, J. L. Stollery
  • Published online by Cambridge University Press:
    04 July 2016, pp. 51-55

  • Hypersonic projectiles are sometimes launched using a castellated sabot which links with matching cavities in the missile. After launch and the removal of the sabot the boundary layer over the vehicle flows past these cavities which act as a kind of roughness. Experiments were made to discover the effect of this ‘roughness’ on the flow over a flap or flare placed downstream of the cavities. Tests were made with both laminar and turbulent boundary layers, the turbulent flow being induced by vortex generators placed near the nose of the models.

Back matter

  • AER volume 106 issue 1063 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, p. b1
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  • AER volume 106 issue 1061 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, p. b1
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  • AER volume 106 issue 1059 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, p. b1
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  • AER volume 106 issue 1060 Cover and Back matter

  • Published online by Cambridge University Press:
    04 July 2016, p. b1
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Other

Front matter

  • AER volume 106 issue 1064 Cover and Front matter

  • Published online by Cambridge University Press:
    04 July 2016, pp. f1-f4
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  • AER volume 106 issue 1062 Cover and Front matter

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

  • Integrated engine management: a new approach to health monitoring and control of gas turbine aero-engines

  • J. J. Gribble, G. J. Dadd
  • Published online by Cambridge University Press:
    04 July 2016, pp. 203-209

  • Integrated engine management (IEM) is a technique for unifying and improving the control and health monitoring of gas turbine aeroengines by increasing the quality and quantity of information available about the engine's health and performance. The core of the system is a real-time engine simulation whose outputs are compared continuously with those of the real engine. Any differences between the predicted and measured outputs are attributed to inaccuracy in the simulation's component performance parameters (such as the compressor efficiencies) which are continuously trimmed to make the outputs of the simulation track those of the real engine. The result is a real-time simulation whose input-output behaviour matches that of the real engine very closely.

Page 5 of 6