An Investigation of Supersonic Store Interference in the Vicinity of a 22 Degree Swept Wing Fuselage Configuration at Mach Numbers of 1.61 and 2.01

Author: Geier, Douglas J.
Year: 1958
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57L18
Link: https://digital.library.unt.edu/ark:/67531/metadc53117/

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