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Evaluation of Heat Transfer Coefficient from Velocity Distribution in Boundary LayerThis paper describes a method of evaluating heat transfer coefficient from a velocity distribution in the boundary layer. The power law velocity profile and universal velocity distribution in a smooth pipe have been used to evaluate the wall shear stress, and the heat transfer coefficient was evaluated from the wall shear stress using the Chilton-Colburn analogy. The predicted pressure drop was compared with the pressure drop computed by the Colebrook equation, and the predicted heat transfer coefficient was compared with the heat transfer coefficient calculated by the Dittus-Boelter equation. The accuracy of pressure drop prediction was within 1%, and the accuracy of heat transfer coefficient prediction was within 8%. This method has the potential to use a Navier-Stokes based CFD solution to evaluate the heat transfer coefficient in nodal or network flow codes.
Document ID
20220016332
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Alok Majumdar
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
October 28, 2022
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: JANNAF LPS/SPS/PIB meeting
Location: Huntsville, Alabama
Country: US
Start Date: December 5, 2022
End Date: December 9, 2022
Sponsors: Joint Army-Navy-NASA-Air Force (JANNAF)
Funding Number(s)
WBS: 012873.05.02.01.62
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Heat Transfer Coefficient
CFD
Nodal Code
Universal Velocity Distribution
Boundary Layer
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