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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