{"title":"Interaction of strong shock waves with perforated stainless-steel plate in a shock tube","authors":"Sergey Golovastov, Grigory Bivol, Fyodor Kuleshov","doi":"10.1007/s00348-025-04051-8","DOIUrl":null,"url":null,"abstract":"<div><p>The results of an experimental study of the attenuation of strong shock waves in a channel during interaction with perforated steel plates with permeability from 0.11 to 0.39 are presented. The experiments were carried out in a shock tube equipped with piezoelectric pressure transducers at initial nitrogen pressures of 10 kPa, 20 kPa and 50 kPa. Mach numbers of the shock waves were varied from 1.5 to 4.3. The pressures of the incident shock waves, reflected shock waves and transmitted shock waves were determined. Graphs of the Mach numbers of reflected and transmitted shock waves depending on the Mach number of the incident shock wave were obtained. The dependence of the attenuation of the transmitted and reflected shock waves on the Mach number of the incident shock wave and on the permeability was obtained. It was shown that the time of pressure relaxation time behind the reflected shock wave increases with increasing Mach number.</p></div>","PeriodicalId":554,"journal":{"name":"Experiments in Fluids","volume":"66 6","pages":""},"PeriodicalIF":2.5000,"publicationDate":"2025-05-29","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Experiments in Fluids","FirstCategoryId":"5","ListUrlMain":"https://link.springer.com/article/10.1007/s00348-025-04051-8","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
引用次数: 0
Abstract
The results of an experimental study of the attenuation of strong shock waves in a channel during interaction with perforated steel plates with permeability from 0.11 to 0.39 are presented. The experiments were carried out in a shock tube equipped with piezoelectric pressure transducers at initial nitrogen pressures of 10 kPa, 20 kPa and 50 kPa. Mach numbers of the shock waves were varied from 1.5 to 4.3. The pressures of the incident shock waves, reflected shock waves and transmitted shock waves were determined. Graphs of the Mach numbers of reflected and transmitted shock waves depending on the Mach number of the incident shock wave were obtained. The dependence of the attenuation of the transmitted and reflected shock waves on the Mach number of the incident shock wave and on the permeability was obtained. It was shown that the time of pressure relaxation time behind the reflected shock wave increases with increasing Mach number.
期刊介绍:
Experiments in Fluids examines the advancement, extension, and improvement of new techniques of flow measurement. The journal also publishes contributions that employ existing experimental techniques to gain an understanding of the underlying flow physics in the areas of turbulence, aerodynamics, hydrodynamics, convective heat transfer, combustion, turbomachinery, multi-phase flows, and chemical, biological and geological flows. In addition, readers will find papers that report on investigations combining experimental and analytical/numerical approaches.