Air entrainment can become a significant problem in a web handling process line. The development of an air film between a roller and web can cause a reduction in traction. This can cause a velocity difference between the web and roller and may also cause guiding problems. Roller grooving is a common method to reduce the effects of the air entrainment to improve traction. A traction simulation model for circumferentially grooved rollers has been devised. The model is based on classical plate and shell theory, the Reynolds’ equation, and asperity contact theory. The governing equations are solved in an iterative scheme using a finite difference method with a variable mesh. Theoretical results are experimentally verified. [S0742-4787(00)02203-7]
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July 2000
Technical Papers
A Numerical Algorithm for Determining the Traction Between a Web and a Circumferentially Grooved Roller
K. S. Ducotey,
K. S. Ducotey
Web Handling Research Center, Dept. of Mechanical & Aerospace Engineering, Oklahoma State University, Stillwater, OK 74078
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J. K. Good
J. K. Good
Web Handling Research Center, Dept. of Mechanical & Aerospace Engineering, Oklahoma State University, Stillwater, OK 74078
Search for other works by this author on:
K. S. Ducotey
Web Handling Research Center, Dept. of Mechanical & Aerospace Engineering, Oklahoma State University, Stillwater, OK 74078
J. K. Good
Web Handling Research Center, Dept. of Mechanical & Aerospace Engineering, Oklahoma State University, Stillwater, OK 74078
Contributed by the Tribology Division for publication in the ASME JOURNAL OF TRIBOLOGY. Manuscript received by the Tribology Division September 16, 1999; revised manuscript received February 8, 2000. Associate Technical Editor: J. Fre^ne.
J. Tribol. Jul 2000, 122(3): 578-584 (7 pages)
Published Online: February 8, 2000
Article history
Received:
September 16, 1999
Revised:
February 8, 2000
Citation
Ducotey , K. S., and Good, J. K. (February 8, 2000). "A Numerical Algorithm for Determining the Traction Between a Web and a Circumferentially Grooved Roller ." ASME. J. Tribol. July 2000; 122(3): 578–584. https://doi.org/10.1115/1.555404
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