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Dilution Jet Behavior in the Turn Section of a Reverse Flow CombusterMeasurements of the temperature field produced by a single jet and a row of dilution jets issued into a reverse flow combustor are presented. The temperature measurements are presented in the form of consecutive normalized temperature profiles, and jet trajectories. Single jet trajectories were swept toward the inner wall of the turn, whether injection was from the inner or outer wall. This behavior is explained by the radially inward velocity component necessary to support irrotational flow through the turn. Comparison between experimental results and model calculations showed poor agreement due to the model's not including the radial velocity component. A widely spaced row of jets produced trajectories similar to single jets at similar test conditions, but as spacing ratio was reduced, penetration was reduced to the point where the dilution jet flow attached to the wall.
Document ID
19820011346
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Riddlebaugh, S. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Lipshitz, A.
(Ahuza Haifa, Israel)
Greber, I.
(Case Western Reserve Univ. Cleveland, Ohio, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 82-0192
E-1107
NASA-TM-82776
Report Number: AIAA PAPER 82-0192
Report Number: E-1107
Report Number: NASA-TM-82776
Meeting Information
Meeting: Aerospace Sci. Meeting
Location: Orlando, FL
Country: United States
Start Date: January 10, 1982
End Date: January 14, 1982
Sponsors: AIAA
Accession Number
82N19220
Funding Number(s)
PROJECT: RTOP 505-15-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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