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Investigation of Spoilers at a Mach Number of 1.93 to Determine the Effects of Height and Chordwise Location on the Section Aerodynamic Characteristics of a Two-Dimensional Wing
Author:
Mueller, James N.
Year:
1958
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-4180
Link:
https://digital.library.unt.edu/ark:/67531/metadc57052/
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