2009
DOI: 10.1007/s10494-009-9203-5
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Recent German Research on Periodical Unsteady Flow in Turbomachinery

Abstract: The main source of flow unsteadiness in turbomachinery is the aerodynamical interaction of the rotor and stator blade rows. The blades and vanes, moving relatively to each other, interact because of the viscous wakes and the potential effects of the blades. In addition, the wakes and potential effects superimpose with other flow patterns, for instance the tip clearance vortices and other secondary flow phenomena. Furthermore in transonic compressors the interaction of wakes and shocks plays an important role. … Show more

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Cited by 4 publications
(1 citation statement)
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“…While in current design processes the flow is mostly considered in its temporal average [11], the real flow in axial compressors and turbines is strongly unsteady, with turbulence and periodic contributions resulting from the aerodynamic interaction of the blade rows moving relative to each other [12][13][14][15]. It exhibits high complexity due to the inner and outer sidewalls and the effects generated by rotation.…”
Section: Introductionmentioning
confidence: 99%
“…While in current design processes the flow is mostly considered in its temporal average [11], the real flow in axial compressors and turbines is strongly unsteady, with turbulence and periodic contributions resulting from the aerodynamic interaction of the blade rows moving relative to each other [12][13][14][15]. It exhibits high complexity due to the inner and outer sidewalls and the effects generated by rotation.…”
Section: Introductionmentioning
confidence: 99%