A study has been made to determine the aerodynamic characteristics of a low-aspect ratio cruciform missile model with all-movable wings and tails. The configuration was tested at Mach numbers from 1.50 to 4.63 with the wings in the vertical and horizontal planes and with the wings in a 45 deg roll plane with all-movable wings and tails. The configuration was tested at Mach numbers from 1.50 to 4.63 with the wings in the vertical and horizontal planes and with the wings in a 45 deg roll plane with tails in line and interdigitated. (Author)
Supersonic Aerodynamic Characteristics of a Low-Aspect-Ratio Missile Model with Wing and Tail Controls and with Tails in Line and Interdigitated
1972
274 pages
Report
No indication
English