... to the square of the blade lift coefficient multiplied by 0.18 26 C D – sec = 0.18 C L – blade 2 07 09 2006 29 09 2006 07 09 2010 07 09 2010 gas turbines flow simulation computational fluid dynamics mechanical engineering computing compressors CAD...

... analysis are reported in Fig. 15 . 13 February 2002 01 May 2003 27 09 2006 transonic flow optimisation computational fluid dynamics CAD turbines compressors Numerical optimization techniques seem to be a promising tool for the aerodynamic design of new generation...

.... This paper looks at that process from the point of view of identifying any bottlenecks and argues that current research should be directed at the CAD-to-mesh-to-solution cycle time rather than, as has been traditional, just looking at the solver itself and in isolation. Work aimed at eliminating some...