This article is an, as no other articles. Please to this page from; try the for suggestions. (February 2014) () Compressor characteristic is the curve to show the behaviour of fluid, like change in pressure, temperature, entropy, flow rate etc. As it passes through a Dynamic compressor at different compressor speeds. The function of a compressor is to increase the pressure of a fluid passing through it, so that the exit pressure is higher than the inlet pressure. Due to this property, compressors are used in a wide range of machines, such as refrigerators, cars, jet engines and industrial processes. These curves are plotted between various parameters and some are as follows.

• Klassen, H.A., `Performance of low pressure ratio centrifugal compressors with four diffuser designs`, NACA, TN 7237, March 1973. Et al., `Effect of Reynolds number on performance characteristics of centrifugal compressors with special reference to configurations of impellers`, ASME paper No.74-GT-59, 1974. • ^ Yahya,S.M, ”Turbine, Compressors & Fans”,4TH ED.McGraw Hill,2011. • Horlock, J.H., Axial Flow Turbines, Kruger Publishing Co., 1973. • Horlock, J.H., Axial Flow Compressors, Kruger Publishing Co., 1973.

Compressor performance and the connect- ed process system's influence on compres- sor capacity. Centrifugal compressors have perfor- mance curves similar.

• Ferguson, T.B., The Centrifugal Compressor Stage, Butterworth, London, 1963. • Whitfield, A. And Wallace, F.J., `Study of incidence loss models in radial and mixed flow turbomachinery`, Instn. Conference Publication, 3, paper No. C55/73, 1973.

• Watanabi, I. And Sakai, T., `Effect of the cone angle of the impeller hub of the mixed flow compressor upon performance characteristics`, SAE paper No.

• Whitfield, A. And Wallace, F.J., `Performance prediction for automotive turbocharger compressors`, Proc.

• Greitzer, E.M., `Surge and rotating stall in axial flow compressors`, ASME J. 2, April 1967. • Tsui, Chih-Ya et al., ` An experiment to improve the surge margin by use of cascade with splitter blades`, J. Thermophys,, Vol. • • Cumpsty, N.

Compressor Aerodynamics. The present basis of axial flow compressor design: Part 1, Cascade theory and performance.

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