Abstract
The problem of nozzle design in transonic flow is difficult because the governing equations are of mixed type, changing from elliptic in the low speed region near the nozzle entry to hyperbolic in the supersonic region near the exit.
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© 1964 Springer-Verlag OHG., Berlin/Göttingen/Heidelberg
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Holt, M. (1964). The design of plane and axisymmetric nozzles by the method of integral relations. In: Oswatitsch, K. (eds) Symposium Transsonicum. International Union of Theoretical and Applied Mechanics (IUTAM) / Internationale Union für Theoretische und Angewandte Mechanik (IUTAM). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-88337-8_20
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DOI: https://doi.org/10.1007/978-3-642-88337-8_20
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-48450-6
Online ISBN: 978-3-642-88337-8
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