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Longitudinal Stability and Control Characteristics of a Canard Missile Configuration for Mach Numbers From 1.1 to 1.93 as Determined From Free-Flight and Wind-Tunnel Investigation
Author:
Curfman, Howard J., Jr.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L52F06
Link:
https://digital.library.unt.edu/ark:/67531/metadc59232/
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