Tests in the Ames 40- by 80-foot wind tunnel of an airplane configuration with a variable-incidence triangular wing and an all-movable horizontal tail

Author: Koenig, David G.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-A53D21
Link: https://digital.library.unt.edu/ark:/67531/metadc59606/

< New search