Titlebook: Experimental Methods of Shock Wave Research; Ozer Igra,Friedrich Seiler Book 2016 Springer International Publishing Switzerland 2016 Exper

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Hypersonic Ludwieg Tubelunt and slender configurations. Furthermore, in order to enable testing of laminar and turbulent flows, the facility should provide a Reynolds-number of 20 Million, based on the model length. The test time should be in the order of 100 ms in order to allow for a range of useful flow measurement tec

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Ozer Igra,Friedrich SeilerWell structured encyclopedic book.Presents a state-of the art overview on Experimental methods of Shock Wave Research.Vol. 9 of the Shock Waves Science and Technology Reference Library.Includes supple

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Shock Wave Science and Technology Reference Libraryhttp://image.papertrans.cn/e/image/318879.jpg

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Vicente Cortés,Klaus Kröncke,Jan LouisA shock tube is a facility that can produce transmitted shock waves in controlled laboratory conditions. The facility is a duct divided into two sections as shown schematically in Fig. 1. One part, the driver, accommodates high pressure gas (P.) while the other section (the driven) contains the low pressure test gas (P.).

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Introduction

Development of the New Piston-Driven Shock-Tunnel HELMThe simulation of high enthalpy, hypersonic flows is a field of continued research efforts and provides a difficult task despite all progress made in the past years.

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