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Aerodynamic Characteristics of a Circular Cylinder at Mach Number 6.86 and Angles of Attack Up to 90 Degrees
Author:
Penland, Jim A.
Year:
1957
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3861
Link:
https://digital.library.unt.edu/ark:/67531/metadc56263/
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