Unique Testing Capabilities of the NASA Langley Transonic ...
This paper examines the use of a Variable Camber Continuous Trailing Edge Flap. (VCCTEF) system for aeroservoelastic optimization of a transport wingbox.
This paper examines the use of a Variable Camber Continuous Trailing Edge Flap. (VCCTEF) system for aeroservoelastic optimization of a transport wingbox.