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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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