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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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