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The effect of velocity overshoot on the performance of magnetohydrodynamic subsonic diffusersThe effect of velocity overshoot, a velocity distribution encountered in magnetohydrodynamic channels with peak velocity near the wall instead of at the center, on the performance of two-dimensional subsonic diffusers was investigated. For the simplified conditions analyzed in this paper it was found that the ratio of peak-to-centerline velocity increases along the diffuser for a diffuser half angle greater than some critical value. It was also found that irrespective of the accompanying inlet temperature distribution the wall shear stress and the wall heat flux is substantially larger when the inlet velocity profile has an overshoot than that for a fully developed turbulent inlet velocity profile.
Document ID
19800035135
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Greywall, M. S.
(Wichita State University Wichita, Kan., United States)
Smith, J. M.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 10, 2013
Publication Date
January 1, 1980
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 80-0251
Report Number: AIAA PAPER 80-0251
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Pasadena, CA
Start Date: January 14, 1980
End Date: January 16, 1980
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
80A19305
Distribution Limits
Public
Copyright
Other

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