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An expansion tube study of high enthalpy carbon-dioxide flows

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Shock Waves

Abstract

A super-orbital expansion tube was used to generate moderate and high enthalpy chemically reacting carbon-dioxide flows. The flow over a cylinder was imaged using holographic interferometry and the density and electron concentrations were determined. Fast response thermocouples were used to measure the stagnation point heat flux. A simple one-dimensional model of the flow was used to calculate values for comparison.

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References

  1. T.J. Mclntyre, A.I. Bishop, A.M. Thomas, A. Sasoh, H. Rubinsztein-Dunlop: Ionizing nitrogen and air flows in a superorbital expansion tube. AIAA Journal 38(9), 1685 (2000)

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  2. T.J. Mclntyre, A.I. Bishop, H. Rubinsztein-Dunlop, P.A. Gnoffo: Experimental and numerical studies of ionizing flow in a super-orbital expansion tube. AIAA Journal 41(11), 2157 (2002)

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  3. A.J. Neely, R.G. Morgan: The superorbital expansion tube concept, experiment and analysis. Aero J. 98, 97 (1994)

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  4. T.J. Mclntyre, M.J. Wegener, A.I. Bishop, H. Rubinsztein-Dunlop: Simultaneous two-wavelength holographic interferometry in a superorbital expansion tube facility. Applied Optics 36(31), 8128 (1997)

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  5. I. Lourel, R.G. Morgan: Fast response coaxial type-E thermocouples for the measurement of heat transfer in hypersonic facilities. Report 2001/05, The Department of Mechanical Engineering, The University of Queensland, Brisbane, Australia (2001)

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  6. T.J. McIntyre, I. Lourel, T.N. Eichmann, R.G. Morgan, P.A. Jacobs, A.I. Bishop: An experimental expansion tube study of the flow over a toroidal ballute. Accepted for publication in Journal of Spacecraft and Rockets (2003)

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© 2005 Tsinghua University Press and Springer-Verlag Berlin Heidelberg

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Mclntyre, T.J., Eichmann, T.N., Lourel, I., Hajek, K.M., Rubinsztein-Dunlop, H. (2005). An expansion tube study of high enthalpy carbon-dioxide flows. In: Jiang, Z. (eds) Shock Waves. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-27009-6_12

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  • DOI: https://doi.org/10.1007/978-3-540-27009-6_12

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-540-22497-6

  • Online ISBN: 978-3-540-27009-6

  • eBook Packages: Physics and AstronomyPhysics and Astronomy (R0)

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