Low-speed longitudinal stability and lateral-control characteristics of a model of a 40 degree swept-wing fighter-type airplane at a Reynolds number of 9 x 10(exp 6)

Author: Bollech, Thomas V.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L54B17
Link: https://digital.library.unt.edu/ark:/67531/metadc60199/

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