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Pressure measurements on cone surface in 3-D shock reflection processes

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Abstract.

In a shock tube the pressure distribution was measured on a cone with an angle of attack when a shock wave passed the cone. The cone has a semi-apex angle of 35°, the angle of attack varied from 0° to 25° and the shock Mach numbers from 1.05 to 3.0. A series of pressure distributions on the cone circumference are given.

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Authors and Affiliations

  1. Stosswellenlabor, RWTH Aachen, Templergraben 55, 52056 Aachen, Germany , , , , , , DE

    H. Zhao & H. Grönig

  2. Dept. of Modern Mech., Univ. of Sci. and Tech. of China, Hefei, Anhui, 230026, P.R. China , , , , , , CN

    X.Z. Yin

Authors
  1. H. Zhao
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  2. X.Z. Yin
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  3. H. Grönig
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Additional information

Received 17 November 1997 / Accepted 5 December 1997

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Zhao, H., Yin, X. & Grönig, H. Pressure measurements on cone surface in 3-D shock reflection processes. Shock Waves 9, 419–422 (1999). https://doi.org/10.1007/s001930050172

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  • DOI: https://doi.org/10.1007/s001930050172

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