Demo
    Close-up image of a Hercules beetle with a shiny, yellow, spot-patterned shell and long, curved horns on a plain white background.
    A small aircraft with
    A modified Gulfstream III was the test bed for Adaptive Compliant Trailing Edge research carried out by NASA and the U.S. Air Force Research Laboratory in California. The accordion-like structure avoids sharp edges to to join FlexSys Inc.'s flexible flap to the wing.
    Close-up view of an aircraft wing's trailing edge with a sharp, streamlined design against a dark background.
    A FlexFoil load alleviation control surface, activated by an internal electric motor, bends upward in a lab demonstration, just as it would do to counteract wing loading from winglets on a KC-135.
    Diagram explaining the process of weakening or preventing sonic booms with lasers. Shows pulse of laser, ionization of air, and interaction of plasma and shock waves around a supersonic aircraft.
    Diagram of a KC-135 plane with annotations showing winglet, load alleviation control surface, and aileron. Text box provides specifications and manufacturer details.
    Adding winglets would improve fuel efficiency of the U.S. Air Force’s refueling tankers, but would impart excessive loads on the wings during maneuvers. FlexSys Inc. hopes to flight test a possible solution under, ALACS, the Active Load Alleviation Control Surface program.
    Close-up of a seal's face with its eyes closed, showing whiskers and a dark, wet nose, partially submerged in water.
    Comparative image under 2.50x magnification shows three seal hair samples: Elephant Seal, California Sea Lion, and Harbor Seal, with a labeled scale for measurement (P = periodicity, R = radius).
    Microscopic comparison of three type of seal whiskers. “P” is the pitch, or distance between peaks. “R” and “a” indicate major axis length.
    A transparent plastic enclosure with various instruments and gauges inside, including a large round dial. Textiles are draped over some of the instruments.
    A 3D-printed seal whisker blade is mounted for testing in a low-speed tunnel. The blade made of thermoplastic polymer and 30 times the size of a normal whisker is the vertical black item to the right of the gauges in the background.
    A row of white curved objects, each labeled with a red letter, are placed on a reflective surface near a cluttered workbench with tools and papers.
    A wavy blade design based on a harbor seal whisker was tested among reference blades in a transonic wind tunnel at NASA’s Glenn Research Center. Test blades are geometrically larger than real turbine blades to better characterize the flow physics.