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


如何引用文章

全文:

开放存取 开放存取
受限制的访问 ##reader.subscriptionAccessGranted##
受限制的访问 订阅存取

详细

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.

作者简介

O. Mirova

Joint Institute for High Temperatures

编辑信件的主要联系方式.
Email: mittelster@gmail.com
俄罗斯联邦, Moscow, 127412

A. Kotel’nikov

Joint Institute for High Temperatures

Email: mittelster@gmail.com
俄罗斯联邦, Moscow, 127412

V. Golub

Joint Institute for High Temperatures

Email: mittelster@gmail.com
俄罗斯联邦, Moscow, 127412

T. Bazhenova

Joint Institute for High Temperatures

Email: mittelster@gmail.com
俄罗斯联邦, Moscow, 127412

补充文件

附件文件
动作
1. JATS XML

版权所有 © Pleiades Publishing, Ltd., 2016