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Shock tube study of the drag coefficient of a sphere in a nonstationary flow

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Shock Waves

Abstract

A shock tube facility was used for inducing relatively high acceleration on small spheres laid on the shock tube floor. The acceleration resulted from the drag force imposed by the post shock wave flow. Using double exposure holography, the sphere trajectory could be constructed accurately. Based upon such trajectories, the sphere drag coefficient was evaluated for a relatively wide range of Reynolds numbers (6000≤ Re ≤ 101000). It was found that the value obtained for the sphere drag coefficient were significantly larger than those obtained in a similar steady flow case.

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© 1992 Springer-Verlag Berlin Heidelberg

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Igra, O., Takayama, K. (1992). Shock tube study of the drag coefficient of a sphere in a nonstationary flow. In: Takayama, K. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-77648-9_77

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  • DOI: https://doi.org/10.1007/978-3-642-77648-9_77

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-77650-2

  • Online ISBN: 978-3-642-77648-9

  • eBook Packages: Springer Book Archive

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