Research Article
Dec 1972
Wind Load on Cylinder with Spanwise Protrusion
Authors: David F. James and Quan-Si TruongAuthor Affiliations
Publication: Journal of the Engineering Mechanics Division
Volume 98, Issue 6
Abstract
Drag and lift forces for circular cylindrical bodies with two types of spanwise protrusions were measured in a wind tunnel in the transition range of Reynolds numbers (104 to 105), with the protrusion size varying from 0.004 to 0.006 of the cylinder diameter. The data show that the two protuberance shapes, a trip-wire and an overlap, are nearly identical in their effect on the aerodynamic characteristics, and that their effect depends much more on location than on size. It was found that the drag coefficient could vary by ±40% and that the lift coefficient could be as high as 0.7, depending on the location of the protuberance, or equivalently on the angle of attack. By using hot-wire anemometry to study the flow field, these significant variations in CD and CL were revealed to be associated with fundamental changes in the boundary-layer flow, caused by the interaction of the protrusion with the surrounding fluid motion.
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Published In
Journal of the Engineering Mechanics Division
Volume 98 • Issue 6 • December 1972
Pages: 1573 - 1589
Copyright
© 1972 American Society of Civil Engineers.
History
Published in print: Dec 1972
Published online: Feb 3, 2021
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Affiliations
David F. James
Assoc. Prof., Dept. of Mech. Engrg., Univ. of Toronto, Toronto, Canada.
Quan-Si Truong
Grad. Student, Dept. of Mech. Engrg., Univ. of Toronto, Toronto, Canada.
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