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The Effect of Base Bleed on the Base Pressure, Lift, Drag, and Pitching Moment of a 10-Percent-Thick Blunt-Base Airfoil at a Mach Number of 2.72
Author:
Jones, Jim J.
Year:
1955
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L54K10
Link:
https://digital.library.unt.edu/ark:/67531/metadc60787/
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