NASA programs developing next-generation aircraft, such as the Subsonic Fixed Wing Project, would benefit from the technology developed in this SBIR program to achieve passive aerodynamic tailoring of wing structures. A similar approach could be implemented using DMLS to create all-metal structures with highly tailored cellular substructures to produce thin, aeroelastically tailored wings for supersonic aircraft, including The Supersonic Project's research in airframe aerodynamic efficiency.
A manufacturable, low-weight composite sandwich structure with coupled bending-torsional stiffness can be implemented to achieve aeroelastic tailoring in many high-aspect ratio aircraft, including next generation commercial transport aircraft and long-endurance UAS vehicles, including Aurora's own Orion UAS.
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