Summary
An experimental study has been conducted to investigate open and closed cavity configurations with and without fluidic control at transonic and supersonic speeds. The cavity models were of L/D = 2, 6, 11 and 18. The investigation was carried out at Mach numbers of 0.8, 1.4 and 1.7. The passive flow control technique employed wedges of 15°, 30°, 45° and 60° were placed at the leading and trailing edge of each cavity. Pressure measurements, and oil flow, were employed to examine the characteristics of the induced flowfield. Experimental results revealed the basic flow features and defined the cavity flow field types.
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© 2009 Springer-Verlag Berlin Heidelberg
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Lada, C., Kontis, K. (2009). Fluidic control of cavity configurations at transonic and supersonic speeds. In: Hannemann, K., Seiler, F. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-85181-3_76
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DOI: https://doi.org/10.1007/978-3-540-85181-3_76
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-85180-6
Online ISBN: 978-3-540-85181-3
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