Abstract
The attenuation of planar shock waves while propagating through dust-gas suspensions was studied experimentally and numerically. The numerical solution was conducted twice, each time using a different correlation for the dust particle drag coefficient. It was shown that when the Reynolds number is relatively high (Re > 200) the solution based on the nonstationary drag coefficient provides better agreement with experimental findings. Also studied was the post shock pressure signature; good agreement was found between experimental and numerical results until the reflected rarefaction wave, from the driver’s end wall, caught up with the transmitted shock wave in the suspension.
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© 1995 Springer-Verlag Berlin Heidelberg
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Igra, O., Ben-Dor, G., Aizik, F., Gelfand, B. (1995). Experimental and Numerical Investigation of Shock Wave Attenuation in Dust-Gas Suspensions. In: Brun, R., Dumitrescu, L.Z. (eds) Shock Waves @ Marseille III. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-78835-2_7
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DOI: https://doi.org/10.1007/978-3-642-78835-2_7
Publisher Name: Springer, Berlin, Heidelberg
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