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Computation of three-dimensional mixed convective boundary layer flowThe paper presents the numerical solution of heat and mass transfer during cross-flow (orthogonal) mixed convection. In this class of flow, a buoyancy-driven transport in the vertical direction and a forced convective flow in the horizontal direction results in a three-dimensional boundary layer structure adjacent to the plate. The rates of heat and mass transfer are determined by a combined influence of the two transport processes. The equations for the conservation of mass, momentum, energy, and species concentration were solved along with appropriate boundary conditions to determine the distributions of velocity components, temperature, and concentration across the thickness of the boundary layer at different locations on the plate. Results were expressed in dimensionless form using Reynolds number, Richardson number for heat transfer, Richardson number for mass transfer, Prandtl number, and Schmidt number as parameters. It was found that the transport is dominated by buoyancy at smaller vertical locations and at larger distances away from the forced convection leading edge. Effects of forced convection appeared to be very strong at smaller horizontal distances from the leading edge. The cross stream forced convection enhanced the rate of heat and mass transfer by a very significant amount.
Document ID
19950020926
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Prashandt Gadepalli
(University of South Florida Tampa, United States)
Muhammad M Rahman
(University of South Florida Tampa, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: The Sixth Annual Thermal and Fluids Analysis Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
NASA-CP-10161
Meeting Information
Meeting: The Sixth Annual Thermal and Fluids Analysis Workshop
Location: Brook Park, OH
Country: US
Start Date: August 15, 1994
End Date: August 19, 1994
Sponsors: National Aeronautics and Space Administration, Ohio Aerospace Institute
Accession Number
95N27347
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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