Summary
The paper presents the method enabling the solution of so called indirect theory problem of blade cascades in case when the flowing medium is an ideal gas, inlet Mach number is supersonic and outlet Mach number subsonic. The supersonic part of the blade cascade is designed by the method of characteristics and the subsonic part by the hodograph method.
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Literature
Busemann, A.: Beitrag Gasdynamik in Wiens-Harms: Handbuch der Experimentalphysik, Bd 4, 1. Teil, Leipzig 1931
Germain, P., Bader, R.: Problème de Dirichlet pour une equation du type mixte. Comptes Rendus, Ac. Sci. Paris, Vol. 238 /1950/
Bergman, S.: On Representation of Stream Functions of Subsonic and Supersonic Flows of Compressible Fluids. Journ. of Rat. Mech. and Analysis, Vol. 4, 1955
Legendre, R.: Calcul Approximatif d’ une grille d’ aubes transonique. La récherche Aéronautique, No. 53, Septembre — Octobre 1956.
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© 1976 Springer-Verlag, Berlin/Heidelberg
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Růžička, M. (1976). Mathematical Method of Designing a Certain Compressor Type Plane Blade Cascade. 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_38
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DOI: https://doi.org/10.1007/978-3-642-81005-3_38
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-81007-7
Online ISBN: 978-3-642-81005-3
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