Abstract
We demonstrate an end-to-end computational model of the HEG shock tunnel as a way to extract more precise test flow conditions and as a way of getting predictions of new operating conditions. For a selection of established operating conditions, the Lid program was used to simulate the one-dimensional gas-dynamic processes within the whole of the facility. The program reproduces the compression tube performance reliably and, with the inclusion of a loss factor near the upstream-end of the compression tube, it provides a good estimate of the equilibrium pressure in the shock-reflection region over the set of six standard operating conditions for HEG.
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© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg
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Jacobs, P.A., Gardner, A.D., Buttsworth, D.R., Martinez Schramm, J., Karl, S., Hannemann, K. (2005). End-to-end modelling of the HEG shock tunnel. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_46
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DOI: https://doi.org/10.1007/978-3-540-27009-6_46
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