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   <subfield code="a">10.1007/s11630-013-0662-6</subfield>
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   <subfield code="a">Temporal behaviour of a corner separation in a radial vaned diffuser of a centrifugal compressor operating near surge</subfield>
   <subfield code="h">[Elektronische Daten]</subfield>
   <subfield code="c">[A. Marsan, I. Trébinjac, S. Coste, G. Leroy]</subfield>
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   <subfield code="a">The temporal behaviour of a flow separation in the hub-suction side corner of a transonic diffuser is studied thanks to unsteady numerical simulations based on the phase-lagged approach. The validity of the numerical results is confirmed by comparison with experimental unsteady pressure measurements. An analysis of the instantaneous skin-friction pattern and particles trajectories is presented. It highlights the topology of the separation and its temporal behaviour. The major result is that, despite of a highly time-dependent core flow, the separation is found to be a &quot;fixed unsteady separation” characterized by a fixed location of the main saddle of the separation but an extent of the stall region modulated by the pressure waves induced by the impeller-diffuser interaction.</subfield>
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   <subfield code="a">Science Press, Institute of Engineering Thermophysics, CAS and Springer-Verlag Berlin Heidelberg, 2013</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Corner Separation</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Radial Vaned Diffuser</subfield>
   <subfield code="2">nationallicence</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Centrifugal Compressor</subfield>
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   <subfield code="a">Surge</subfield>
   <subfield code="2">nationallicence</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">N1 : Number of blades in the impeller</subfield>
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   <subfield code="a">N2 : Number of blades in the radial vaned diffuser</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">Ω [rad/s] : Rotation speed of the impeller</subfield>
   <subfield code="2">nationallicence</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">T1 : Temporal period of the flow in the impeller</subfield>
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   <subfield code="a">T2 : Temporal period of the flow in the diffuser</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">T0[○K] : Total temperature</subfield>
   <subfield code="2">nationallicence</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">p0 [Pa] : Total pressure</subfield>
   <subfield code="2">nationallicence</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">P : Static pressure</subfield>
   <subfield code="2">nationallicence</subfield>
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  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">$$\vec v$$ : Flow velocity vector</subfield>
   <subfield code="2">nationallicence</subfield>
  </datafield>
  <datafield tag="690" ind1=" " ind2="7">
   <subfield code="a">$$\dot m\left[ {kg/s} \right]$$ : Massflow</subfield>
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   <subfield code="a">Cp : Static pressure recovery coefficient of the diffuser</subfield>
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   <subfield code="a">K : Total pressure loss coefficient of the diffuser</subfield>
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   <subfield code="a">Marsan</subfield>
   <subfield code="D">A.</subfield>
   <subfield code="u">Laboratoire de Mécanique des Fluides et d'Acoustique, UMR CNRS 5509 École Centrale de Lyon, 69134, Ecully, France</subfield>
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