Abstract
For the design of turbomachines as a whole, as well as for individual stages, and to understand the performance of stages, certain similarity rules are used. For this purpose, the following notations are used:
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References
B. Eckert, Axial- und Radial Kompressoren (Springer, Berlin, 1953)
W. Traupel, Thermische Turbomaschinen, vol. 1 (Springer, Berlin, 1966)
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© 2012 Springer Science+Business Media, LLC
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Bose, T. (2012). Similarity Rules (on Design Condition). In: Airbreathing Propulsion. Springer Aerospace Technology. Springer, New York, NY. https://doi.org/10.1007/978-1-4614-3532-7_6
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DOI: https://doi.org/10.1007/978-1-4614-3532-7_6
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