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Structural response of an advanced combustor liner: Test and analysisAn advanced (segmented) combustor liner supplied by Pratt and Whitney Aircraft was tested in the structural component test rig at Lewis Research Center. It was found that the segmented liner operated at much lower temperatures than the conventional liner (about 400 F lower) for the same heat flux. At the lower temperatures and low thermal gradients, little distortion to the segments was observed. The operating conditions were not severe enough to distort or damage the segmented liner.
Document ID
19890007958
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Moorhead, Paul E.
(NASA Lewis Research Center Cleveland, OH., United States)
Thompson, Robert L.
(NASA Lewis Research Center Cleveland, OH., United States)
Tong, M.
(Sverdrup Technology, Inc., Cleveland OH., United States)
Higgins, M.
(Sverdrup Technology, Inc., Cleveland OH., United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Publication Information
Publication: Turbine Engine Hot Section Technology, 1987
Subject Category
Structural Mechanics
Accession Number
89N17329
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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