Abstract:
In this investigation, the numerical solutions of
Navier-Stokes equations and energy equation are presented for (1)
laminar free slot jet, (ii) laminar free axisymmetric jet, (iii)
laminar jet impingement on a circular cylinder, (iv) vertically
downward laminar slot jet impinging on a flat surface with and
without buoyancy, and (v) offset slot jet in the range. of low
Reynolds numbers for both, the uniform and the parabolic slot-exit
velocity and temperature profiles. SIMPLE and SIMPLEC algorithm
have been used for the numerical solutions.
The velocity and temperature profiles are presented near the
nozzle-exit and far away from the nozzle-exit plane for free slot
jet and free axisymmetric jet. The centreline velocity and
temperature become coincident for all Reynolds numbers when
plotted against R= X/Re. The velocity profiles become coincident
for all Reynolds numbers far away from nozzle-exit in
Schlichting's variable ii and with half jet width as characteristic
length. The results are in good agreement with the available
experimental results. The jet diffuses at a fast rate at lower
Reynolds numbers and the jet spread decreases at higher Reynolds
numbers.
Jet impingement over a cylinder has been investigated for low
Reynolds numbers. The results for skin friction, pressure
distribution and velocity profiles on cylinder surface, are
presented. The results do not depend strongly on slot width. The
effect of decrease in slot -to-cylinder spacing is equivalent to
increase in Reynolds number. The flow separation occurs earlier at
vi i
higher Reynolds numbers.
In case of vertically downward slot jet impinging on a flat
surface, the buoyancy force significantly affects the flow field,
the local Nusselt number, local friction factor and the pressure
distribution along the impingement surface. The jet behaves almost
like a non-buoyant jet for values of Richardson numbers less than
0.014 with uniform slot-exit profiles and Richardson number less
than 0.007 with parabolic slot-exit profiles. The jet detaches
from the surface and rises up like a plume for Ri 0.014 with
uniform slot-exit profiles and for Ri 0.007 with parabolic
slot-exit profiles. The jet does not come into contact with the
surface at all for Ri 1.25 for both, the uniform and parabolic
slot-exit profiles. Empirical correlations have been developed for
determining the average Nusselt number, maximum Nusselt number and
the stagnation point Nusselt number for both the types of velocity
and temperature profiles in absence of buoyancy for laminar flow.
The maximum Nusselt number occurs at the stagnation point for
parabolic slot-exit profiles, whereas for uniform slot-exit
profiles, it occurs slightly away from the stagnation point.
The offset ratio significantly influences the 1ocalNusselt
number, local friction factor and the pressure along the
impingement surface for offset slot jet in the range of low
Reynolds numbers. Secondary recirculation is observed at an offset
ratio of 7 and Reynolds number of 80. The reattachment length is
observed to be approximately constant at higher values of Reynolds
numbers. Empirical correlations have been developed for the
reattachment length, maximum Nusselt number and the average Nusselt number in the separated region.
Description:
This thesis is submitted to the Department of Mechanical Engineering, Indian Institute of Technology, Kharagpur, India in partial fulfillment of the requirements for the degree of
Doctor of Philosophy in Engineering, 1996.
Cataloged from PDF Version of Thesis.
Includes bibliographical references (pages 373-387).