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Incidence and Deviation

  • Meinhard T. SchobeiriEmail author
Chapter

Abstract

Up to this point, the relationships developed for a turbomachinery stage have been strictly correct for given velocity diagrams with known inlet and exit flow angles. We assumed that the flow is fully congruent with the blade profile.

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References

  1. 1.
    Gostelow, J. P., 1984, “Cascade Aerodynamics,” Pergamon Press.Google Scholar
  2. 2.
    Scholz, N, 1965, “Aerodynamik der Schaufelgitter,” Brwon-Verlag, Karlsruhe.Google Scholar
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    Betz, A., 1948, “Konforme Abbildung,” Berlin, Göttingen, Springer-Verlag.CrossRefGoogle Scholar
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    Weinig, F., 1935, “Die Strömung um die Scahufeln von Turbomaschinen,” Leipzig, Barth-Verlag.zbMATHGoogle Scholar
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    Eckert, B., Schnell, E., 1961, “Axial-und Radialkompressoren,” 2. Auflage, Berlin, Göttingen, Heidelberg, Springer-Verlag.CrossRefGoogle Scholar

Copyright information

© Springer Nature Switzerland AG 2019

Authors and Affiliations

  1. 1.Department of Mechanical EngineeringTexas A&M UniversityCollege StationUSA

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