The laminar boundary layer flow when a two-dimensional slot jet impinges on a flat plate at some angle is analyzed theoretically. The conservation equations in primitive variables are solved using a finite-difference technique. The computed results at 0 and 90 deg angle of impingement are in perfect agreement with the standard solutions available in the literature. The influence of the angle of impingement on the velocity and temperature profiles is studied. The presence of a stagnation point when the plate is not parallel to the oncoming jet is found to affect considerably the local Nusselt number and skin friction coefficient. These parameters attain very large values close to the stagnation point at small angles of impingement. However, far from the stagnation point, they approach values corresponding to a flat plate at zero incidence, irrespective of the angle of jet impingement.
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Boundary Layer Analysis for Two-Dimensional Slot Jet Impingement on Inclined Plates
V. K. Garg,
V. K. Garg
Department of Mechanical Engineering, Indian Institute of Technology, Kanpur 208016, India
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S. Jayaraj
S. Jayaraj
Department of Mechanical Engineering, Indian Institute of Technology, Kanpur 208016, India
Search for other works by this author on:
V. K. Garg
Department of Mechanical Engineering, Indian Institute of Technology, Kanpur 208016, India
S. Jayaraj
Department of Mechanical Engineering, Indian Institute of Technology, Kanpur 208016, India
J. Heat Transfer. Aug 1988, 110(3): 577-582 (6 pages)
Published Online: August 1, 1988
Article history
Received:
January 7, 1986
Online:
October 20, 2009
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A commentary has been published:
Closure to “Discussions of ‘Transient Response of Floating Ring Liquid Seals’” (1988, ASME J. Tribol., 110, pp. 577–578)
Citation
Garg, V. K., and Jayaraj, S. (August 1, 1988). "Boundary Layer Analysis for Two-Dimensional Slot Jet Impingement on Inclined Plates." ASME. J. Heat Transfer. August 1988; 110(3): 577–582. https://doi.org/10.1115/1.3250531
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