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NACA0012 with Aileron (Marianna Braza)

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Unsteady Effects of Shock Wave Induced Separation

The IoA Experiment

This study integrates the Institute of Aviation (IoA) experiments and the numerical simulations and turbulence modelling of the University of Liverpool (ULIV)and by the Institut de Mécanique des Fluides de Toulouse (IMFT). The IoA experiment focused on unsteady flow characteristics and buffet phenomena arising as the result of the shock wave / boundary layer interaction in transonic flow over a NACA 0012 airfoil equipped with an aileron. The transonic buffet is a natural and self-sustaining oscillation of the shock wave and the separated flow region, caused by pressure fluctuation.

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References

  1. Batten, P., Goldberg, U., Chakravarty, S.: Sub-grid turbulence modeling for unsteady flow with acoustic resonance. AIAA Paper No 00–0473 (2000)

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  2. Miller, M., Kania, V.: Parameters for aerofoil and aileron oscillations, UFAST Deliverable D3.1.3 (March 2009)

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  3. Barakos, G., Drikakis, D.: Numerical simulation of transonic buffet flows using various turbulence closures. International Journal of Heat and Fluid Flow 21(5), 620–626 (2000)

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  4. Bourguet, R., Braza, M., Hoarau, Y., Harran, G., El Akoury, R.: AIAA J. (2007); J. Fluids & Struct. (2009)

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© 2010 Springer-Verlag Berlin Heidelberg

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Doerffer, P., Hirsch, C., Dussauge, JP., Babinsky, H., Barakos, G.N. (2010). NACA0012 with Aileron (Marianna Braza). In: Unsteady Effects of Shock Wave Induced Separation. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 114. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-03004-8_4

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  • DOI: https://doi.org/10.1007/978-3-642-03004-8_4

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-03003-1

  • Online ISBN: 978-3-642-03004-8

  • eBook Packages: EngineeringEngineering (R0)

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