Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles

Author: Phelps, E. Ray
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A56B03
Link: https://digital.library.unt.edu/ark:/67531/metadc62823/

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