Abstract
This paper outlines the theory of radical farming in scramjets and describes the experimental scramjet model that was designed to investigate it. Experiments were conducted at two conditions; a 3MJ/kg condition corresponding to Mach 7.9 flight at an altitude of 24km and a 4MJ/kg condition corresponding to Mach 9.1 flight at an altitude of 32km. The results are presented as pressure distributions on the flowpath wall and specific impulse estimates.
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References
A.D. Gardner. Upstream porthole injection in a 2-D scramjet model. Master’s thesis, The University of Queensland, 2000.
C. J. Jachimowski. An analysis of combustion studies in shock expansion tunnels and reflected shock tunnels. Technical Report TP-3224, NASA, 1992.
A. Kovachevich, A. Pauli, and T Mclntyre. Investigation of an intake injected hot-wall scramjet. In 42 nd AIAA Aerospace Sciences Meeting and Exhibit, Nevada, U.S.A., Jan. 2004. AIAA-2004-1037.
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© 2007 Springer-Verlag Berlin Heidelberg
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Odam, J., Paull, A. (2007). Radical Farming in Scramjets. In: Tropea, C., Jakirlic, S., Heinemann, HJ., Henke, R., Hönlinger, H. (eds) New Results in Numerical and Experimental Fluid Mechanics VI. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 96. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-74460-3_34
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DOI: https://doi.org/10.1007/978-3-540-74460-3_34
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-74458-0
Online ISBN: 978-3-540-74460-3
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