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Investigation at High Subsonic Speeds of the Effects of Various Horizontal Fuselage Forebody Fins on the Directional and Longitudinal Stability of a Complete Model Having a 45 Degree Sweptback Wing
Author:
Sleeman, William C., Jr.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56J25
Link:
https://digital.library.unt.edu/ark:/67531/metadc63053/
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