What people are saying - Write a review
We haven't found any reviews in the usual places.
Diagram of defining the matching points using universal curve
d0 0 002
7 other sections not shown
Other editions - View all
alloy analysis angle application ASME average axial balancing blade boundary layer calculated cascade characteristics clearance coefficient compared components compressor constant cooling critical cycle damping described determined developed diffuser direction distribution edge effect efficiency element engine equation exit experimental Figure flow fluid force frequency fuel function Gas Turbine given heat helium increase indicate inlet Journal limit loading loss mass material maximum mean measurements mechanical method mode obtained occur operating passage percent performance phase plane plant position predicted presented pressure probe Products radial range ratio reference region relative response rotating rotor seal shaft shown in Fig shows speed stage static stress surface Table technique temperature transfer tube turbulence values velocity vibration wake wall