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An experimental trace gas investigation of fluid transport and mixing in a circular-to-rectangular transition ductAn ethylene trace gas technique was used to map out fluid transport and mixing within a circular to rectangular transition duct. Ethylene gas was injected at several points in a cross stream plane upstream of the transition duct. Ethylene concentration contours were determined at several cross stream measurement planes spaced axially within the duct. The flow involved a uniform inlet flow at a Mach number level of 0.5. Statistical analyses were used to quantitatively interpret the trace gas results. Also, trace gas data were considered along with aerodynamic and surface flow visualization results to ascertain transition duct flow phenomena. Convection of wall boundary layer fluid by vortices produced regions of high total pressure loss in the duct. The physical extent of these high loss regions is governed by turbulent diffusion.
Document ID
19910017815
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Reichert, B. A.
(NASA Lewis Research Center Cleveland, OH., United States)
Hingst, W. R.
(NASA Lewis Research Center Cleveland, OH., United States)
Okiishi, T. H.
(Iowa State Univ. of Science and Technology Ames., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 91-2370
NAS 1.15:104499
E-6356
NASA-TM-104499
Meeting Information
Meeting: Joint Propulsion Conference
Location: Sacramento, CA
Country: United States
Start Date: June 24, 1991
End Date: June 27, 1991
Sponsors: ASME, SAE, ASEE, AIAA
Accession Number
91N27129
Funding Number(s)
PROJECT: RTOP 505-62-91
Distribution Limits
Public
Copyright
Public Use Permitted.
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