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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/metadc53140/
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