Summary
Steady two-dimensional transonic flows of ideal inviscid gases through Laval nozzles are computed by a method based on the numerical methods of Telenin [2], Pirumov [6], and Hopkins and Hill [3]. Both the direct and inverse problems are treated for plane and axisymmetric nozzles. Numerical results are compared to the experimental results of Cuffel et al. [8] and results obtained by other numerical methods, namely series and relaxation solutions.
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References
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© 1976 Springer-Verlag, Berlin/Heidelberg
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Klopfer, G.H., Holt, M. (1976). Steady Transonic Flow through Plane and Axisymmetric Nozzles. In: Oswatitsch, K., Rues, D. (eds) Symposium Transsonicum II. International Union of Theoretical and Applied Mechanics. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-81005-3_42
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DOI: https://doi.org/10.1007/978-3-642-81005-3_42
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-81007-7
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