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Wind-Tunnel Investigation of the Effects of a Jet Engine Nacelle on the Aerodynamic Characteristics of a 37.25 Degree Swept Back Wing at High Subsonic Speeds
Author:
Boltz, Frederick W.
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-A50H23
Link:
https://digital.library.unt.edu/ark:/67531/metadc58607/
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