Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98

Author: Perkins, Edward W.
Additional Authors: Gowen, Forrest E.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A51G13
Link: https://digital.library.unt.edu/ark:/67531/metadc59005/

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