Abstract
A device has been produced which can detect the contamination of the test gas by the driver gas in a reflected shock tunnel. This device monitors the static pressure in a converging duct. The duct is designed to choke at a predetermined contamination level due to the change in the specific heat ratio produced by the contaminants. Experimental results are given for a freestream enthalpy of nominally 6 MJ/kg.
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Hornung H, Sturtevant B, Belanger J, Sanderson S, Brouillette M, Jenkins M (1991) Performance data of the new free-piston shock tunnel T5 at GALCIT. Shock Waves Proc. K.Takayama (ed). 1 pp 603–610
Lordi JA, Mates RE, Moselle JR (1966) Computer program for numerical simulation of nonequilibrium expansions of reacting gas mixtures. NASA CR-472
McIntosh MK (1968) Computer program for the numerical calculation of frozen and equilibrium conditions in shock tunnels. Dept. of Phys. Aust. Nat. Univ. Australia
Skinner KA (1994) Mass spectrometry in shock tunnel experiments of hypersonic combustion. Ph.D. thesis Univ. of Qld. Australia
Stalker RJ, Morgan RG (1988) The University of Queensland's free piston shock tunnel — initial operation and preliminary calibration. 4th Nat. Space Symp. Adelaide 12–14 July
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Paull, A., King, M.D. A driver gas detection device for shock tunnels. Shock Waves 4, 289–291 (1995). https://doi.org/10.1007/BF01416041
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DOI: https://doi.org/10.1007/BF01416041