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Effects of a Fuselage on the Aerodynamic Characteristics of a 42 Degree Sweptback Wing at Reynolds Numbers to 8,000,000
Author:
Salmi, Reino J.
Additional Authors:
Conner, D. William
Year:
1947
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L7E13
Link:
https://digital.library.unt.edu/ark:/67531/metadc64565/
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