德国航空航天中心哥廷根高焓冲击隧道

J. Martinez Schramm, Alexander Wagner, D. Surujhlal, Giannino Ponchio Camillo
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引用次数: 0

摘要

德国航空航天中心(DLR)的哥廷根高焓冲击隧道(HEG)是欧洲主要的高超音速试验设施之一。它于 1991 年投入使用,此后被广泛用于大量国家和国际太空和高超音速飞行项目。该设施最初是为研究高温效应(如化学和热弛豫)对进入或重返大气层的太空飞行器空气热力学的影响而设计的。在过去的几年中,其工作条件范围不断扩大。在这一框架内,主要重点是生成测试条件,以便能够在较宽的高度范围内研究从低空 6 马赫到 10 马赫的高超音速飞行构型的流动情况。在 HEG 中进行的研究侧重于外部和内部空气动力学,包括超音速燃烧中的氢气燃烧、冲击波边界层相互作用、调查和控制高超音速流动和高超音速湍流中的边界层过渡。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
High Enthalpy Shock Tunnel Göttingen of the German Aerospace Center (DLR)
The High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) is one of the major European hypersonic test facilities. It was commissioned for use in 1991 and was utilized since then extensively in a large number of national and international space and hypersonic flight projects. Originally, the facility was designed for the investigation of the influence of high temperature effects such as chemical and thermal relaxation on the aerothermodynamics of entry or re-entry space vehicles. Over the last years its range of operating conditions was subsequently extended. In this framework the main emphasis was to generate test conditions which allow investigating the flow past hypersonic flight configurations from low altitude Mach 6 up to Mach 10 in a wide altitude range. The studies performed in HEG focused on external as well as internal aerodynamics including combustion of hydrogen in supersonic combustion, shock-wave boundary layer interaction, the investigation and control of boundary layer transition in hypersonic flows and hypersonic turbulence.
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