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Effects of Step Shape on Transition over a Swept Backward-Facing StepThe effect of backward-facing step shape on stationary-crossflow growth was studied down-stream of a two-dimensional step in a swept-wing flow. The step height was set at 76% of the local unperturbed boundary-layer thickness at the step location, and the shape was varied by placing three ramps of differing slopes and shapes on the downstream face of the step, including a 30◦ramp, rounded ramp, and a 5◦ramp. In addition, the square step shape (with noramp) was studied. The 5◦ramp was the only one that was successful at substantially delaying transition downstream of the step. Even so, it did not completely mitigate the effect of the step. The 5◦ramp significantly altered the mean flow, significantly reducing the separation region downstream of the step. While this geometry still resulted in increased growth of the stationary crossflow instability, it substantially reduced the amplitude of the unsteady instabilities that grew downstream of the step. In particular, this ramp completely eliminated the low-frequency, traveling crossflow mode that was observed in the other cases.
Document ID
20200011448
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Jenna L Eppink
(Langley Research Center Hampton, Virginia, United States)
Date Acquired
May 21, 2020
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-34696
Report Number: NF1676L-34696
Meeting Information
Meeting: AIAA Aviation 2020
Location: Virtual
Country: US
Start Date: June 15, 2020
End Date: June 19, 2020
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.07.05.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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