End-to-end modelling of the HEG shock tunnel
Contribuinte(s) |
Zonglin Jiang |
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Data(s) |
01/01/2004
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Resumo |
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 L1d 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. |
Identificador | |
Idioma(s) |
eng |
Publicador |
Springer |
Palavras-Chave | #Free-piston Driver #EX #290201 Aerodynamics #671401 Scientific instrumentation |
Tipo |
Conference Paper |