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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