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A theory of post-stall transients in multistage axial compression systemsA theory is presented for post stall transients in multistage axial compressors. The theory leads to a set of coupled first-order ordinary differential equations capable of describing the growth and possible decay of a rotating-stall cell during a compressor mass-flow transient. These changing flow features are shown to have a significant effect on the instantaneous compressor pumping characteristic during unsteady operation, and henace on the overall system behavior. It is also found from the theory that the ultimate mode of system response, stable rotating stall or surge, depends not only on the B parameter but also on other parameters, such as the compressor length-to-diameter ratio. Small values of this latter quantity tend to favor the occurrence of surge, as do large values of B. A limited parametric study is carried out to show the impact of the different system features on transient behavior. Based on analytical and numerical results, several specific topics are suggested for future research on post-stall transients.
Document ID
19850012807
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Moore, F. K.
(Cornell Univ. Ithaca, NY, United States)
Greitzer, E. M.
(Cornell Univ. Ithaca, NY, United States)
Date Acquired
September 5, 2013
Publication Date
March 1, 1985
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:3878
NASA-CR-3878
Report Number: NAS 1.26:3878
Report Number: NASA-CR-3878
Accession Number
85N21117
Funding Number(s)
CONTRACT_GRANT: NAG3-34
CONTRACT_GRANT: NSG-3208
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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