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TECHNICAL PAPERS

Lateral Deflections of Webs in Air-Flotation Ovens

[+] Author and Article Information
Peter M. Moretti

School of Mechanical and Aerospace Engineering, Oklahoma State University, Stillwater, OK 74078-5016e-mail: moretti@ceat.okstate.edu

J. Appl. Mech 71(3), 314-320 (Jun 22, 2004) (7 pages) doi:10.1115/1.1756922 History: Received March 12, 2001; Revised November 03, 2003; Online June 22, 2004
Copyright © 2004 by ASME
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References

Figures

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Nomenclature; the sine wave is drawn with exaggerated amplitude—actual amplitudes are small, and zbar may be negative
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Relationship between web curvature y and pressure distribution p, both shown as functions of x
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Deflection shape, y/L versus x/L, from Eq. (39), the low-elasticity equilibrium solution for a cambered web, for full-width-traction at the exit, with unit camber parameter (Eq. (32))
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Deflection shape from Eq. (41), the low-elasticity equilibrium solution for a cambered web, for partial-slip at the exit roller (dotted line) for a high value of 8 for the tension/beam-parameter (Eq. (43)), compared with full-width-traction at the exit (solid line)
Grahic Jump Location
Deflection shape from Eq. (41), the low-elasticity equilibrium solution for a cambered web, for partial-slip at the exit roller (dotted line) for a low value of 3.7 for the tension/beam-parameter (Eq. (43)), compared with full-width-traction at the exit (solid line)

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