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Investigation of the Jet Effects on a Flat Surface Downstream of the Exit of a Simulated Turbojet Nacelle at a Free-Stream Mach Number of 2.02
Author:
Bressette, Walter E.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54E05a
Link:
https://digital.library.unt.edu/ark:/67531/metadc62524/
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