Using the theory developed in Part I, calculations have been carried out to show the evolution of the mass flow, pressure rise, and rotating-stall cell amplitude during compression system post-stall transients. In particular, it is shown that the unsteady growth or decay of the stall cell can have a significant effect on the instantaneous compressor pumping characteristic and hence on the overall system behavior. A limited parametric study is carried out to illustrate the impact of different system features on transient behavior. It is shown, for example, that the ultimate mode of system response, surge or stable rotating stall, depends not only on the B parameter, but also on the compressor length-to-radius ratio. Small values of the latter quantity tend to favor the occurrence of surge, as do large values of B. Based on the analytical and numerical results, some specific topics are suggested for future research on post-stall transients.
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April 1986
Research Papers
A Theory of Post-Stall Transients in Axial Compression Systems: Part II—Application
E. M. Greitzer,
E. M. Greitzer
Massachusetts Institute of Technology, Cambridge, MA
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F. K. Moore
F. K. Moore
Cornell University, Ithaca, NY
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E. M. Greitzer
Massachusetts Institute of Technology, Cambridge, MA
F. K. Moore
Cornell University, Ithaca, NY
J. Eng. Gas Turbines Power. Apr 1986, 108(2): 231-239 (9 pages)
Published Online: April 1, 1986
Article history
Received:
January 10, 1985
Online:
October 15, 2009
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Citation
Greitzer, E. M., and Moore, F. K. (April 1, 1986). "A Theory of Post-Stall Transients in Axial Compression Systems: Part II—Application." ASME. J. Eng. Gas Turbines Power. April 1986; 108(2): 231–239. https://doi.org/10.1115/1.3239893
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