Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of the Sidewinder Missile at Mach Numbers from 1.2 to 2.1

Author: Brown, Clarence A., Jr.
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SL55K16
Link: https://digital.library.unt.edu/ark:/67531/metadc65501/

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