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Investigation of the Aerodynamic Characteristics of the NACA RM-10 Missile (With Fins) at a Mach Number of 1.62 in the Langley 9-Inch Supersonic Tunnel
Author:
Coletti, Donald E.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52J23a
Link:
https://digital.library.unt.edu/ark:/67531/metadc279567/
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