End-to-end modelling of the HEG shock tunnel


Autoria(s): Jacobs, P. A.; Gardner, A. D.; Buttsworth, D. R.; Schramm, J. M.; Karl, S.; Hannemann, K.
Contribuinte(s)

Zonglin Jiang

Data(s)

01/01/2004

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

http://espace.library.uq.edu.au/view/UQ:100898

Idioma(s)

eng

Publicador

Springer

Palavras-Chave #Free-piston Driver #EX #290201 Aerodynamics #671401 Scientific instrumentation
Tipo

Conference Paper