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CFD Mixing Analysis of Jets Injected from Straight and Slanted Slots into Confined Crossflow in Rectangular DuctsA CFD study was performed to analyze the mixing potential of opposed rows of staggered jets injected into confined crossflow in a rectangular duct. Three jet configurations were numerically tested: (1) straight (0 deg) slots; (2) perpendicular slanted (45 deg) slots angled in opposite directions on top and bottom walls; and (3) parallel slanted (45 deg) slots angled in the same direction on top and bottom walls. All three configurations were tested at slot spacing-to-duct height ratios (S/H) of 0.5, 0.75, and 1.0; a jet-to-mainstream momentum flux ratio (J) of 100; and a jet-to-mainstream mass flow ratio of 0.383. Each configuration had its best mixing performance at S/H of 0.75. Asymmetric flow patterns were expected and predicted for all slanted slot configurations. The parallel slanted slot configuration was the best overall configuration at x/H of 1.0 for S/H of 0.75.
Document ID
19920017318
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bain, D. B.
(CFD Research Corp. Huntsville, AL., United States)
Smith, C. E.
(CFD Research Corp. Huntsville, AL., United States)
Holdeman, J. D.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1992
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.15:105699
E-7087
AIAA PAPER 92-3087
NASA-TM-105699
Report Number: NAS 1.15:105699
Report Number: E-7087
Report Number: AIAA PAPER 92-3087
Report Number: NASA-TM-105699
Meeting Information
Meeting: Joint Propulsion Conference and Exhibit
Location: Nashville, TN
Country: United States
Start Date: July 6, 1992
End Date: July 8, 1992
Sponsors: ASEE, ASME, SAE, AIAA
Accession Number
92N26561
Funding Number(s)
PROJECT: RTOP 537-02-20
Distribution Limits
Public
Copyright
Public Use Permitted.
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