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Wave Processes in Transonic Airfoil Flows

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28th International Symposium on Shock Waves

Introduction

Upstream moving pressure waves are observed in transonic flows over airfoils already for decades. They can be generated actively by flap or airfoil oscillations [6]. But, they are also naturally present in airfoil flows [1, 4]. Upstream moving pressure waves can lead to flow instabilities by forcing shock and stagnation point oscillations. Furthermore, it is expected that they affect the laminar-turbulent transition [5]. Hence, the phenomenon is of great engineering interest.

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References

  1. Alshabu, A., Olivier, H.: Unsteady wave phenomena on a supercritical airfoil. AIAA J. 46(8), 2066–2073 (2008)

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  4. Lee, B.H.K., Murty, H.: Role of Kutta waves on oscillatory shock motion on an airfoil. AIAA J. 32(4), 789–796 (1994)

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  5. Seiler, F., Srulijes, J.: Vortices and pressure waves at trailing edges. In: Proc. of 16th Intern. Cong. on High Speed Photography and Photonics, Strasbourg, France (1984)

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  6. Tijdemann, H.: Investigation of the transonic flow around oscillating airfoils, NLR TR-77090 (1977)

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© 2012 Springer-Verlag Berlin Heidelberg

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Hermes, V., Nies, J., Klioutchnikov, I., Olivier, H. (2012). Wave Processes in Transonic Airfoil Flows. In: Kontis, K. (eds) 28th International Symposium on Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-25685-1_76

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  • DOI: https://doi.org/10.1007/978-3-642-25685-1_76

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-25684-4

  • Online ISBN: 978-3-642-25685-1

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