A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2018; you can also visit the original URL.
The file type is application/pdf
.
Unsteady Boundary-Layer Transition in Flow Periodically Disturbed by Wakes
1992
Volume 1: Turbomachinery
unpublished
Boundary layers on turbomachinery blades develop in a flow which is periodically disturbed by the wakes of upstream blade cascades. These wakes have a significant effect upon laminar-turbulent boundary-layer transition. In order to study these effects, detailed velocity measurements using hot-wire probes were performed within the boundary-layer of a plate in flow periodically disturbed by wakes produced by bars moving transversal to the flow. The measurements were evaluated using the
doi:10.1115/92-gt-283
fatcat:mpdidvfqubcthchvjbnx6awczy