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Transonic Flight Tests to Determine Zero-Lift Drag and Pressure Recovery of Nacelles Located at the Wing Root on a 45 Degree Sweptback Wing and Body Configuration
Author:
Hoffman, Sherwood
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53H20
Link:
https://digital.library.unt.edu/ark:/67531/metadc59707/
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