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Effect of axially staged fuel introduction on performance of one-quarter sector of annular turbojet combustor
Author:
Zettle, Eugene V.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E53A28
Link:
https://digital.library.unt.edu/ark:/67531/metadc59600/
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