Abstract
The flow past hypersonic vehicles causes large heat loads on the vehicle surfaces. It is shown that the heat loads and the flow properties are strongly coupled, if radiation cooling is employed. Similar phenomena occur in interacting flows, and in non-equilibrium viscous flows. The large demands on ground-facility simulation of hypersonic flows make new ways in experimental work necessary. A Hot Experimental Technique, each for three different typical measurement problems, is pro-posed. Details of the technique, regarding the tunnel type, model and measurement techniques are discussed. A stepwise approach to the involved problems is suggested.
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© 1993 Springer Science+Business Media Dordrecht
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Hirschel, E.H. (1993). Hot Experimental Technique: a New Requirement of Aerothermodynamics. In: Boutier, A. (eds) New Trends in Instrumentation for Hypersonic Research. NATO ASI Series, vol 224. Springer, Dordrecht. https://doi.org/10.1007/978-94-011-1828-6_3
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DOI: https://doi.org/10.1007/978-94-011-1828-6_3
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-4807-1
Online ISBN: 978-94-011-1828-6
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