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Wind-Tunnel Tests of a Model of a Wingless Fin-Controlled Missile to Obtain Static Stability and Control Characteristics Through a Range of Mach Numbers From 0.5 to 0.88
Author:
Burrows, Dale L.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L53J06
Link:
https://digital.library.unt.edu/ark:/67531/metadc62754/
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