Tests in the Ames 40- by 80-foot wind tunnel of an airplane model with an aspect ratio 4 triangular wing and an all-movable horizontal tail - high-lift devices and lateral controls

Author: Franks, Ralph W
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A52K13
Link: https://digital.library.unt.edu/ark:/67531/metadc59454/

< New search