NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Analysis of Developing Laminar Flows in Circular Pipes Using a Higher-Order Finite-Difference TechniqueA higher-order finite-difference technique is developed to calculate the developing-flow field of steady incompressible laminar flows in the entrance regions of circular pipes. Navier-Stokes equations governing the motion of such a flow field are solved by using this new finite-difference scheme. This new technique can increase the accuracy of the finite-difference approximation, while also providing the option of using unevenly spaced clustered nodes for computation such that relatively fine grids can be adopted for regions with large velocity gradients. The velocity profile at the entrance of the pipe is assumed to be uniform for the computation. The velocity distribution and the surface pressure drop of the developing flow then are calculated and compared to existing experimental measurements reported in the literature. Computational results obtained are found to be in good agreement with existing experimental correlations and therefore, the reliability of the new technique has been successfully tested.
Document ID
19950020931
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Herbert J Gladden
(Lewis Research Center Cleveland, OH, United States)
Ching L Ko
(Oakland University Rochester, United States)
Douglas E Boddy
(Oakland University Rochester, 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
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
95N27352
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
No Preview Available