The Effect of Axial Velocity Ratio, Turbulence Intensity, Incidence, and Leading Edge Geometry on the Midspan Performance of a Turbine Cascade
CANADIAN AERONAUTICS AND SPACE JOURNAL ; 39 , 3 ; 150
1993-01-01
150 pages
Aufsatz (Zeitschrift)
Unbekannt
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Leading-Edge Endwall Suction and Midspan Blowing to Reduce Turbomachinery Losses
Online Contents | 2010
|Influence of Sweep on Axial Flow Turbine Aerodynamics at Midspan
Online Contents | 2007
|Turbulence Amplification with Incidence at the Leading Edge of a Compressor Cascade
Online Contents | 1999
|British Library Conference Proceedings | 2009
|