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Weight-flow and thrust limitations due to use of rotating combustors in a turbojet engine
Author:
Lezberg, Erwin A.
Additional Authors:
Blackshear, Perry L., Jr.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E55K16
Link:
https://digital.library.unt.edu/ark:/67531/metadc61872/
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