Efficiency of wind fences is evaluated by the reduction of wind velocity and the effective shelter area behind the fence. Fence porosity is the most influential structural parameters in the...

Main feature of the ESFVC is that it uses Variable Camber Continuous Trailing Edge Flap (VCC-TEF) flight control surfaces to bend & twist the wing to a "drooped wing" configuration that was …

Main feature of the ESFVC is that it uses Variable Camber Continuous Trailing Edge Flap (VCC-TEF) flight control surfaces to bend & twist the wing to a "drooped wing" configuration that was …

Jun 1, 2014 · This paper reports the results of a computational study that was conducted to explore the effect of various Variable Camber Continuous Trailing Edge Flap (VCCTEF) …

The Variable Camber Continuous Trailing Edge Flap (VCCTEF) wing is a concept of current interest for a design that would allow, if validated, improvements in aircraft performance...

To address the performance aspects of wing flexibil-ity in transport design, NASA developed an innovative wing shaping control concept called the variable cam-ber continuous trailing edge …

Use the VCCTEF to twist the flexible wing to obtain changes in lift-to-drag ratios that will reduce cruise drag throughout the flight envelope. Determine aeroelastic control approaches that will …

Sep 15, 2015 · This paper summarizes the recent development of an adaptive aeroelastic wing shaping control technology called variable camber continuous trailing edge flap (VCCTEF).

Jun 13, 2014 · Session: Special Session: Aerodynamic-Structural Modeling, Optimization, and Test Techniques for Flexible Wing Technology I.

On the basis of a VCCTEF (variable camber continuous trailing edge flap) system which is feasible in engineering, this paper constructs the corresponding mechanical model and …