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.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
Preview
Unable to display preview. Download preview PDF.
References
Batten, P., Goldberg, U., Chakravarty, S.: Sub-grid turbulence modeling for unsteady flow with acoustic resonance. AIAA Paper No 00–0473 (2000)
Miller, M., Kania, V.: Parameters for aerofoil and aileron oscillations, UFAST Deliverable D3.1.3 (March 2009)
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)
Bourguet, R., Braza, M., Hoarau, Y., Harran, G., El Akoury, R.: AIAA J. (2007); J. Fluids & Struct. (2009)
Rights and permissions
Copyright information
© 2010 Springer-Verlag Berlin Heidelberg
About this paper
Cite this paper
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
Download citation
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)