Transonic free-flight investigation of the longitudinal aerodynamic characteristics of a 1/10-scale steel-wing of the Northrop MX-775A missile with leading-edge extensions, inboard trailing-edge flaps, and a speed brake on the vertical tail

Author: Arbic, Richard G
Year: 1955
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SL55B07
Link: https://digital.library.unt.edu/ark:/67531/metadc61180/

< New search