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Liner environment effects studyThe Liner Environment Effects Study Program is aimed at establishing a broad heat transfer data base under controlled experimental conditions by quantifying the effects of the combustion system conditions on the combustor liner thermal loading and on the flame radiation characteristics. Five liner concepts spanning the spectrum of liner design technology from the very simple to the most advanced concepts are investigated. These concepts comprise an uncooled liner, a conventional film cooled liner, an impingement/film cooled liner, a laser drilled liner approaching the concept of a porous wall, and a siliconized silicon carbide ceramic liner. Effect of fuel type is covered by using fuels containing 11.8, 12.8, and 14% hydrogen. Tests at 100, 200, and 300 psia provide a basis for evaluating the effect of pressure on the heat transfer. The effects of the atomization quality and spray characteristics are examined by varying the fuel spray Sauter mean diameter and the spray angle. Additional varied parameters include reference velocity, a wide range of equivalence ratio, cooling flow rate, coolant temperature and the velocity of the coolant stream on the backside of the liner.
Document ID
19840012488
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Venkataramani, K. S.
(General Electric Co. Philadelphia, PA, United States)
Ekstedt, E. E.
(General Electric Co. Philadelphia, PA, United States)
Date Acquired
August 11, 2013
Publication Date
April 1, 1984
Publication Information
Publication: NASA. Lewis Research Center Combust. Fundamentals Res.
Subject Category
Aircraft Propulsion And Power
Accession Number
84N20556
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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