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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