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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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