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Free-flight investigation of the full-scale Hughes Falcon missile, D configuration, to determine aileron effectiveness and damping in roll
Author:
Lundstrom, Reginald R.
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-SL54K19
Link:
https://digital.library.unt.edu/ark:/67531/metadc61010/
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