Investigations on an axial flow fan stage subjected to circumferential inlet flow distortion and swirl
Author:
Publisher
Springer Science and Business Media LLC
Subject
Condensed Matter Physics
Link
http://link.springer.com/content/pdf/10.1007/s11630-997-0003-8.pdf
Reference7 articles.
1. Aulehla, F., “Intake Swirl-a Major Disturbance Parameter in Engine/Intake Compatibility,” ICAS-82-4.8.1, (1982).
2. Ehrich, F., “Circumferential Inlet Distortions in Axial Flow Turbomachinery,” Journal of the Aeronautical Sciences, 24, pp.413–417, (1957).
3. Colpin, J., “Propagation of Inlet Flow Distortions through an Axial Compressor Stage,” ASME Journal of Engineering for Power, 101, pp.116–124, (1979).
4. Yocum, A.M., and Henderson, R.E., “The Effects of Some Design Parameters of an Isolated Rotor on Inlet Flow Distortions,” ASME Journal of Engineering for Power, 102, pp.178–186, (1980).
5. Cousins, W.T., Dalton, K.K., Anderson, T.T., and Bobula, G.A., “Pressure and Temperature Distortion Testing of a Two Stage Centrifugal Compressor,” Trans. ASME, Journal of Engineering for Gas Turbines and Power, 116, pp.567–573, (1994).
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