home      resources      multimedia      research      personnel
news      events      safety      links      contact
Multimedia
Jason Bourgeois


Centrifugal compressor stage


Velocity triangle at impeller exit


A single passage through the impeller and diffuser


Blade-to-blade relative Mach number contours at 50% span


Blade-to-blade relative Mach number contours at 95% span


Normal-to-centreline planes, showing diffuser Mach number contours

2004 launch, afm/c.dybenko; 2004-2005 maintenance, j.dybenko; 2006-2010 maintenance, w.lin; 2010-2012 maintenance, k.elliott; 2012 - webmaster, s.ali; updated July 2014