Development of High-rate, Adaptive Trailing Edge Control Surface for the Smart Wing Phase 2 Wind Tunnel Model

By Jonathan D. Bartley-Cho, Donny P. Wang, Christopher A. Martin, J. Kudva, M. West. 2004

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Skin design studies for variable camber morphing airfoils (2008, methodology): “Under the DARPA/AFRL/NASA Smart Wing Program, a team led by Northrop-Grumman Corporation used smart materials based technologies to produce smoothly varying leading- and trailing-edge camber in place of standard hinged control surfaces, for improved performance of military aircraft.”
Morphing unmanned aerial vehicles (2011, methodology): “Perera et al have developed a system that uses a torque tube actuation mechanism to enable morphing [38], similar to that developed for the DARPA Smart Wing Project [39].”
Composite corrugated structures for morphing wing skin applications (2010, background): “…projects such as NASA’s Morphing Project (Florance et al 2003, Bartley-Cho et al 2004, Kudva 2004), DARPA’s Smart Wing programme (Florance et al 2003, Bartley-Cho et al 2004, Kudva 2004) and Morphing Aircraft Structures programme (Love et al 2004, Bowman et al 2007, Bye and McClure 2007, Love et…”
Flexible Skins for Morphing Aircraft Using Cellular Honeycomb Cores (2010, background): “…the Mission Adaptive Wing Program (Hall, 1989), the Active Aeroelastic Wing Program (Pendleton et al., 2000), the Smart Wing Program (Kudva, 2004; Bartley-Cho et al., 2004), and most recently, the Morphing Aircraft Structures Program (Andersen et al., 2007; Bowman et al., 2007; Love et al.,…”