Toward improved simulation tools for compressible turbomachinery: assessment of residual-based compact schemes for the transonic compressor NASA Rotor 37

Author: Cinnella P.   Michel B.  

Publisher: Taylor & Francis Ltd

ISSN: 1061-8562

Source: International Journal of Computational Fluid Dynamics, Vol.28, Iss.1-2, 2014-01, pp. : 31-40

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