2007, Volume 1, Issue 4
Frontiers in Energy >> 2007, Volume 1, Issue 4 doi: 10.1007/s11708-007-0063-5
Numerical investigation of aerodynamic performance influenced by circumferentially pre-swirling coming flow on the crossover and de-swirling cascade of a multistage centrifugal compressor
College of Power Engineering, University of Shanghai for Science and Technology, Shanghai 200093, China;
Next Previous
Abstract
Keywords
aerodynamic ; investigation ; centrifugal ; de-swirling ; circumferent
京公网安备 11010502051620号
