Free-Flight Investigation to Determine Force and Hinge-Moment Characteristics at Zero Angle of Attack of a 60 Degrees Sweptback Half-Delta Tip Control on a 60 Degrees Sweptback Delta Wing at Mach Numbers Between 0.68 and 1.44

Author: Martz, C. William
Additional Authors: Church, James D.
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L51I14
Link: https://digital.library.unt.edu/ark:/67531/metadc59056/

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