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Investigation of Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 1.39
Author:
Bressette, Walter E.
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L55L13
Link:
https://digital.library.unt.edu/ark:/67531/metadc61898/
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