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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