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The Longitudinal Stability, Control Effectiveness, and Control Hinge Moment Characteristics Obtained From a Flight Investigation of a Canard Missile Configuration at Transonic and Supersonic Speeds
Author:
Niewald, Roy J.
Year:
1950
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L50I27
Link:
https://digital.library.unt.edu/ark:/67531/metadc58681/
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