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Prediction of turbomachinery flow physics from CFD - review of recent computations of APPACET test cases

Treść / Zawartość
Identyfikatory
Warianty tytułu
Konferencja
Seminar/summer school on "CFD for turbomachinery applications" (01-03.09.2001, Gdańsk, Poland)
Języki publikacji
EN
Abstrakty
EN
In order to maintain a competitive edge, the turbomachinery industry has to rely increasingly on design and analysis methods based on numerical simulation of flow. The European funded APPACET was set up to study the application of turbulence modelling and the simulation of unsteady interactions to provide guidelines for the application of CFD to design. This paper shows the results of computations of four of the test cases studied by the project. The importance of grid refinement has been clearly demonstrated, but no evidence was found that one family of turbulence models could be definitely better than the other. Compared to steady results, unsteady time-averaged solutions have not shown any major improvement in accuracy. However unsteady flow phenomena generating losses within each blade row have been captured and partly explained.
Rocznik
Strony
407--431
Opis fizyczny
Bibliogr. 18 poz., rys., tab.
Twórcy
  • School of Engineering, University of Durham, South Road, DH13LE Durham, UK
  • School of Engineering, University of Durham, South Road, DH13LE Durham, UK
Bibliografia
  • [1] Mathioudakis K, Papailliou K, Neris N, Bonhommet C, Albrand G and Wenger U 1997 An Annular Cascade Facility for Studying Tip-clearance Effects in High Speed Flows XIII ISOABE Chattanooga
  • [2] Bonhommet-Chabanel C and Gerolymos G A 1998 Analysis of Tip Leakage Effects in a High Subsonic Annular Compressor Cascade ASME Paper 98-GT-195
  • [3] Launder B E and Sharma B I 1974 Letters in Heat and Mass Transfer 1 131
  • [4] Craft T J, Launder B E and Suga K 1996 International Journal of Heat and Fluid Flow 17 (2) 108
  • [5] Jones W P and Launder B E 1972 International Journal of Heat and Mass Transfer 15 301
  • [6] Baldwin B and Lomax H 1978 Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows AIAA-78–257
  • [7] Yang Z and Shih H 1993 AIAA Journal 31 (7) 1191
  • [8] AGARD 1998 CFD Validation for Propulsion System Components AGARD-AR-355
  • [9] Strazisar A J 1994 Data Report and Data Diskette for NASA Transonic Compressor Rotor37 NASA Lewis Research Center
  • [10] Shabbir A, Celestina M L, Adamczyk J J and Strazisar A J 1997 The Effect of Hub Leakage Flow on Two High Speed Axial Flow Compressor Rotors ASME Paper 97-GT-346
  • [11] Hah C and Loellbach J 1997 Development of Hub Corner Stall and its Influence on the Performance of Axial Compressor Blade Rows ASME Paper 97-GT-42
  • [12] Arnone A and Pacciani R January 1998 Journal of Turbomachinery 120 147
  • [13] Denton J D 1983 ASME J. of Engineering for Power 105 (3) 514
  • [14] Patel V C, Rodi W and Scheuerer G 1985 AIAA Journal 23 (9) 1308
  • [15] Wallscheid L and Eulitz F 1997 Investigation of Rotor/Rotor Interaction ISABE 97–7186
  • [16] Wallscheid L, Eulitz F and Heinecke R 1998 Investigation of Unsteady Flow Phenomena in a Counterrotating Ducted Propfan ASME 98-GT-251
  • [17] Wallscheid L 1999 Ph¨anomenologische Untersuchung der zeitabh¨angigen Str¨omung in einem gegenl ¨aufigen Propfan DLR-Forschungsbericht 1999–24
  • [18] Gerolymos G A and Vallet I 1997 AIAA Journal 35 228
Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-article-BAT3-0015-0071
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