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Measurements of the Flow Field Within a Compressor Outlet Guide Vane Passage
1993
Volume 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery
unpublished
A series of tests have been carried out to investigate the flow in a Compressor Outlet Guide Vane (OGV) blade row downstream of a single stage rotor. The subsequent flow field that developed within an OGV passage was measured, at intervals of 10% axial chord, using a novel design of miniature 5 hole pressure probe. In addition to indicating overall pressure levels and the growth of regions containing low energy fluid, secondary flow features were identified from calculated axial voracity
doi:10.1115/93-gt-022
fatcat:obwakjm6yfaxjcuojfmadruh5q