Some Features of Tip Gap Flow Fields of a Linear Compressor Cascade

This thesis presents some results from an experimental study of three-dimensional turbulent tip gap flows in the linear cascade wind tunnel, for two different tip gap clearances (t/c=1.65% and 3.3%). The experiments focus on near-wall flow field measurements for the stationary wall and moving wall,...

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Bibliographic Details
Main Author: Tian, Qing
Other Authors: Aerospace and Ocean Engineering
Format: Others
Published: Virginia Tech 2011
Subjects:
LDV
Online Access:http://hdl.handle.net/10919/9673
http://scholar.lib.vt.edu/theses/available/etd-01062004-160730