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Wake Structure Induced by Seal Whisker: Effects of Angle of IncidenceSeal whiskers have been found to produce unique wake flow structures that minimize self-induced vibration and reduce drag. The cause of these wake features are due to the peculiar three-dimensional morphology of the whisker surface. The whisker can be defined as an elliptical cross section with variation in the major and minor axis of the ellipse along the length of the whisker as well as rotation of the elliptical plane with respect to the whisker axis, angle of incidence. While the effects of several dominant parameters of the whisker morphology have been studied, the effect of the rotation of the elliptical plane has not been well understood. This paper will examine the influence of the angle of incidence on the wake flow structure through series of water channel studies. Several models of whisker-like geometries will be tested which isolate the rotation angle as the only variation between models. The wake structure behind each seal whisker model will be measured through particle image velocimetry (PIV). The different models’ wake structures will be compared identifying the effect of angle of incidence on the wake structure. Angle of incidence was found to influence the wake structure through reorganization of velocity patterns, reduction of recovery length and modification of magnitude of Tu. These results help provide a more complete understanding of the seal whisker geometry relationship to wake structure and can provide insight into design practices for application of whisker geometery to various engineering problems.
Document ID
20190027269
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Rinehart, Aidan W.
(Cleveland State Univ. Cleveland, OH, United States)
Zhang, Wei
(Cleveland State Univ. Cleveland, OH, United States)
Shyam, Vikram
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
July 12, 2019
Publication Date
January 9, 2017
Subject Category
Aerodynamics
Report/Patent Number
GRC-E-DAA-TN52934
Meeting Information
Meeting: AIAA Aerospace Sciences Meeting 2017
Location: Grapevine, TX
Country: United States
Start Date: January 9, 2017
End Date: January 13, 2017
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 081876.01.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
vortex induced vibration
Seal Whisker
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