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Corrections for Convective Heat Flux Gauges Subjected to a Surface Temperature DiscontinuityA two-dimensional Navier-Stokes computational fluid dynamics (CFD) analysis has been carried out in an effort to determine the convective heat transfer corrections for circular heat flux gauges subjected to a surface temperature discontinuity. Solutions were obtained at a Reynolds number Of 1 x 10(exp 6) and a Mach number of 4. The CFD results are compared with the existing correlations for the correction factors. In general, the CFD corrections exceed those provided by the correlations. The discrepancy increases with increasing upstream surface temperature, thus indicating the role of property variations, which are not accounted for in the correlations. A quasi-two-dimensional analysis is also performed to treat the cylindrical geometry of the heat flux gauges by area-averaging the computed two-dimensional results from CFD.
Document ID
20020039708
Acquisition Source
Kennedy Space Center
Document Type
Preprint (Draft being sent to journal)
Authors
Kandula, M.
(DYNACS Engineering Co., Inc. Cocoa Beach, FL United States)
Reinarts, T.
(NASA Kennedy Space Center Cocoa Beach, FL United States)
Voska, N.
Date Acquired
August 20, 2013
Publication Date
January 1, 2002
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2002-3087
Meeting Information
Meeting: AIAA/ASME Thermophysics and Heat Transfer Conference
Location: Saint Louis, MO
Country: United States
Start Date: June 24, 2002
End Date: June 27, 2002
Sponsors: American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NAS10-98001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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