Longitudinal Stability and Control Characteristics of an Airplane Model Having a 42.8 Degree Sweptback Circular-Arc Wing With Aspect Ratio 4.00, Taper Ratio 0.50, and Sweptback Tail Surfaces

Author: Weil, Joseph
Additional Authors: Comisarow, Paul
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L7G28
Link: https://digital.library.unt.edu/ark:/67531/metadc58180/

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