Abstract
In a continuous cold gas wind tunnel, with a convergent-divergent nozzle geometry similar to a pilot facility for the gas-phase synthesis of nanoparticles [3] the recompression from supersonic to subsonic flow conditions is conducted by a shock train. A principle sketch of a typical shock train is depicted in Fig. 1 while a detailed description of the shock train phenomenon and a comprehensive review of its timeaveraged behaviour can be found in [6].
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Grzona, A., Weiss, A., Olivier, H. (2015). Modification of Shock Train Induced Turbulence by a Variable Nozzle Opening Angle and Circumferential Suction. In: Bonazza, R., Ranjan, D. (eds) 29th International Symposium on Shock Waves 2. ISSW 2013. Springer, Cham. https://doi.org/10.1007/978-3-319-16838-8_20
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DOI: https://doi.org/10.1007/978-3-319-16838-8_20
Publisher Name: Springer, Cham
Print ISBN: 978-3-319-16837-1
Online ISBN: 978-3-319-16838-8
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