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Development of a turbojet combustor with a segmentally constructed liner Final summary reportAxial and circumferential segmented combustor liners for turbojet engine
Document ID
19690001534
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Biondi, D. (Curtiss-Wright Corp. Wood-Ridge, NJ, United States)
Draizen, S. (Curtiss-Wright Corp. Wood-Ridge, NJ, United States)
Date Acquired
August 5, 2013
Publication Date
June 24, 1968
Subject Category
Propulsion Systems
Report/Patent Number
WAD-R437
NASA-CR-54635
Report Number: WAD-R437
Report Number: NASA-CR-54635
Accession Number
69N10865
Funding Number(s)
CONTRACT_GRANT: NAS3-7908
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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