Modified Surge in an Axial Flow Compressor
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This paper deals with an experimental study of the unsteady flow in a multistage axial-flow compressor with a high design flow coefficient (p = 1.2) at rpm lower than the design ones. A detailed description of the rotating stall during the so-called “modified surge” is given. In this surge type the rotating stall exists during all the surge cycle, in contradistinction of classic surge, when the rotating stall exists only in a part of the surge cycle.
2011 ◽
Vol 20
(1)
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pp. 6-12
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2000 ◽
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1963 ◽
Vol 29
(201)
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pp. 895-902
1978 ◽
Vol 20
(2)
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pp. 101-114
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2009 ◽
Vol 2009
(0)
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pp. 377-378
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2016 ◽
Vol 2016
(0)
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pp. 0914
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2006 ◽
Vol 2006.2
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pp. 149-150
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