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References, Chapter 16
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Lieblein, S., Analysis of experimental low-speed loss and stall characteristics of two-dimensional compressor blade cascades, NACA RM E57A28 March 1957.
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Seylor, D.R., Smith, L.H., Single stage experimental evaluation of high Mach number compressor rotor blading, Part I, Design of rotor blading. NASA CR-54581, GE R66fpd321P, 1967.
Seylor, D.R., Gostelow, J.P., Single stage experimental evaluation of high Mach number compressor rotor blading, Part II, Performance of rotor 1B. NASA CR-54582, GE R67fpd236, 1967.
Gostelow, J.P., Krabacher, K.W., Smith, L.H., Performance comparisons of the high Mach number compressor rotor blading NASA Washington 1968, NASA CR-1256.
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Miller, G.R., Lewis, G.W., Hartman, M.J., Shock losses in transonic compressor blade rows ASME Journal for Engineering and Power July 1961, pp. 235–241.
Schwenk, F.C., Lewis, G.W., Hartmann, M.J., A preliminary analysis of the magnitude of shock losses in transonic compressors NACA RM #57A30 March 1957.
Schwenk, F.C., Lewis, G.W., Hartmann, M.J., A preliminary analysis of the magnitude of shocklosses in transonic compressors NACA RM #57A30 March 1957.
Levine, Ph., Two-dimensional inlet conditions for a supersonic compressor with curved blades, Journal of Applied Mechanics, Vol. 24, No. 2, June 1957.
Balzer, R.L., A method for predicting compressor cascade total pressure losses when the inlet relative Mach number is greater than unity, ASME Paper 70-GT-57.
Swan, W.C., A practical method of predicting transonic compressor performance, ASME Journal for Engineering and Power, Vol. 83, pp. 322–330, July 1961.
Levine, Ph., Two-dimensional inlet conditions for a supersonic compressor with curved blades, Journal of Applied Mechanics, Vol. 24, No. 2, June 1957.
Swan, W.C., A practical method of predicting transonic compressor performance, ASME Journal for Engineering and Power, Vol. 83, pp. 322–330, July 1961.
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Schobeiri, M. (2005). Modeling the Compressor Component, Design and Off-Design. In: Turbomachinery Flow Physics and Dynamic Performance. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-26591-7_16
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