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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