NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Press Enter or click the Search button to begin your search.

Back to Results
A Spreadsheet for the Mixing of Rows of Jets with Confined Crossflow in a Rectangular DuctThis is a printout of the supplemental spreadsheet that is a supplement to the document found in NASA/TM-2010-216100. The calculations for cases of opposed rows of jets with the orifices on one side shifted show that staggering can improve the mixing, particularly for cases where jets would overpenetrate slightly if the orifices were in an aligned configuration.
Document ID
20100030574
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Holderman, James D. (NASA Glenn Research Center Cleveland, OH, United States)
Clisset, James R. (Florida Univ. Gainesville, FL, United States)
Moder, Jeffrey P. (NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
July 1, 2010
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2010-216100/SUPPL
E-17185
Report Number: NASA/TM-2010-216100/SUPPL
Report Number: E-17185
Funding Number(s)
WBS: WBS 561581.02.08.03.16.03
Distribution Limits
Public
Copyright
Public Use Permitted.

Related Records

IDRelationTitle20100029653See AlsoSpreadsheet Calculations for Jets in Crossflow: Opposed Rows of Inline and Staggered Holes and Single and Opposed Rows with Alternating Hole Sizes20100029653Supplemented BySpreadsheet Calculations for Jets in Crossflow: Opposed Rows of Inline and Staggered Holes and Single and Opposed Rows with Alternating Hole Sizes20100029653Supplement ToSpreadsheet Calculations for Jets in Crossflow: Opposed Rows of Inline and Staggered Holes and Single and Opposed Rows with Alternating Hole Sizes
No Preview Available