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Keywords: shock loss
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Proceedings Papers

Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A069, September 21–25, 2020
Paper No: GT2020-16131
... capability. In Part II, the effectiveness of both original and updated models will be tested for one specific low aspect ratio axial compressor stage. Experimental and numerical data will be used at such extent. loss correlations axial compressors profile loss shock loss end-wall loss tip-leakage...
Topics: Compressors
Proceedings Papers

Proc. ASME. GT2020, Volume 2A: Turbomachinery, V02AT32A029, September 21–25, 2020
Paper No: GT2020-14713
... compressors profile loss shock loss end-wall loss tip-leakage loss TRANSONIC AXIAL COMPRESSORS LOSS CORRELATIONS: PART I ANALYSIS AND UPDATE OF LOSS MODELS Marco Manfredi , Fabrizio Fontaneto von Karman Institute for Fluid Dynamics Rhode-Saint-Gene`se, Belgium ABSTRACT The quest for greener, more...
Topics: Compressors
Proceedings Papers

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 569-578, June 3–6, 2002
Paper No: GT2002-30383
..., such as -variant distortion. words: transonic, compressor, cfd, shock loss RODUCTION In general, the application of streamline curvature (SLC) hods to transonic fans has been limited. The SLC oaches do not typically include accurate fundamentally d off-design loss and deviation models (Bloch, et al., 6...
Proceedings Papers

Proc. ASME. GT2002, Volume 5: Turbo Expo 2002, Parts A and B, 23-32, June 3–6, 2002
Paper No: GT2002-30327
... different designs is produced and analysed by CFD. It is found that the 3D features have remarkably little effect on the shock pattern near the tip where the shock must remain perpendicular to the casing. Lower down the blade significant shock sweep, and hence reduced shock loss, can be induced by 3D design...