Investigation of the Effect of Chordwise Positioning and Shape of an Underwing Nacelle on the High-Speed Aerodynamic Characteristics of a 45 Degree Sweptback Tapered-in-Thickness-Ratio Wing of Aspect Ratio 6

Author: Silvers, H. Norman
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L52K25
Link: https://digital.library.unt.edu/ark:/67531/metadc64713/

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