2006
DOI: 10.1098/rspa.2005.1651
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Transition length in turbine/compressor blade flows

Abstract: High Reynolds number mathematical models for convected vortex impinging against a local hump and sound scattering into Tollmien–Schlichting eigenmodes are introduced to simulate basic mechanisms of the disturbance excitation typical of turbomachinery environments. The streamwise dimension of the transitional flow on the suction side of a blade is evaluated on the assumption that the transition length is of equal order with the extent of viscous/inviscid interaction controlling the boundary-layer response. The … Show more

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Cited by 4 publications
(4 citation statements)
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“…As has been mentioned, recent studies [18] and [19] show that the triple-deck approach covers late (deep) transition An experimental correlation reported in [20] for the transition length in turbine blading strictly follows the theoretical prediction based on the triple-deck scaling specified in (2.2a)-(2.2d). Let us elucidate the cause at the heart of this discovery, whence it follows that the extent in the streamwise direction of the nonlinear viscous/inviscid interaction process controlled by the system of Prandtl Eqs.…”
Section: Extension To Transition Analysismentioning
confidence: 73%
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“…As has been mentioned, recent studies [18] and [19] show that the triple-deck approach covers late (deep) transition An experimental correlation reported in [20] for the transition length in turbine blading strictly follows the theoretical prediction based on the triple-deck scaling specified in (2.2a)-(2.2d). Let us elucidate the cause at the heart of this discovery, whence it follows that the extent in the streamwise direction of the nonlinear viscous/inviscid interaction process controlled by the system of Prandtl Eqs.…”
Section: Extension To Transition Analysismentioning
confidence: 73%
“…The range of the triple-deck applicability is broad, though initially the theory was put forward in connection with steady laminar flows. Recent studies [18] and [19] show that this asymptotic approach covers late (deep) transition as well. What is more, an experimental correlation given in [20] for the transition length in turbine blading strictly follows the theoretical prediction based on triple-deck scaling.…”
Section: Introductionmentioning
confidence: 99%
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“…As nitrogen is the main constituent of air and the cycle is closed, pressurisation can be used to ensure Reynolds number similarity with an ABGT compressor, which ingests air at 300 K and 0.1 MPa. Using Equation 9 a UHTS compressor needs to ingest nitrogen at 1790 K and 2.12 MPa to maintain Reynolds number similitude [16] with an ABGT compressor, which typically has a Reynolds number of approximately 650000 [17].…”
Section: Stage 1-2mentioning
confidence: 99%