NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Extensional Flow Convecting a Reactant Undergoing a First Order Homogeneous Reaction and Diffusional Mass Transfer From a Sphere at Low to Intermediate Peclet and Damkohler NumbersForced convective diffusion-reaction is considered for viscous axisymmetric extensional convecting velocity in the neighborhood of a sphere. For Peclet numbers in the range 0.1 ≤ Pe ≤ 500 and for Damkohler numbers increasing with increasing Pe but in the overall range 0.02 ≤ Da ≤ 10, average and local Sherwood numbers have been computed. By introducing the eigenfunction expansion c(r,Θ) = Σ cn(r)Pn(cosΘ) into the forced convective diffusion equation for the concentration of a chemical species undergoing a first order homogeneous reaction and by using properties of the Legendre functions Pn(cosΘ), the variable coefficient PDE can be reduced to a system of N+1 second order ODEs for the radial functions Cn (r), n=0,1,2, ... ,N. The adaptive grid algorithm of Pereyra and Lentini can be used to solve the corresponding 2(N+ 1) first order differential equations as a two-point boundary value problem on 1 ≤ r ≤ r••. Convergence of the expansion for a specific value of N can thus be established and provides "spectral" behavior as well as the full concentration field c(r,Θ).
Document ID
19950020925
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
N Y Shah
(Missouri University of Science and Technology Rolla, United States)
X B Reed, Jr
(Missouri University of Science and Technology Rolla, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Sixth Annual Thermal and Fluids Analysis Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CP-10161
Meeting Information
Meeting: 6th Annual Thermal and Fluids Analysis Workshop
Location: Brook Park, OH
Country: US
Start Date: August 15, 1994
End Date: August 19, 1994
Sponsors: Ohio Aerospace Institute, Glenn Research Center
Accession Number
95N27346
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
No Preview Available