Protecting shield influence on pressure decrease at shock wave interaction with the wall


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Abstract

Pressure decrease is investigated at reflection, from the end of the shock tube channel, of the shock wave passing through its sand layer. The influence of the layer location on the pressure pulse extension and on the decrease of the maximal pressure amplitude behind the shock wave is studied.

About the authors

O. A. Mirova

Joint Institute for High Temperatures

Author for correspondence.
Email: mittelster@gmail.com
Russian Federation, Moscow, 127412

A. L. Kotel’nikov

Joint Institute for High Temperatures

Email: mittelster@gmail.com
Russian Federation, Moscow, 127412

V. V. Golub

Joint Institute for High Temperatures

Email: mittelster@gmail.com
Russian Federation, Moscow, 127412

T. V. Bazhenova

Joint Institute for High Temperatures

Email: mittelster@gmail.com
Russian Federation, Moscow, 127412

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