Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel : influence of trailing-edge flap span and deflection on the longitudinal characteristics

Author: Cancro, Patrick A.
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SL54H27
Link: https://digital.library.unt.edu/ark:/67531/metadc60848/

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