This modified F/A-18A is the test aircraft for the Active Aeroelastic Wing (AAW) project at NASA's Dryden Flight Research Center, Edwards, California.
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This modified F/A-18A is the test aircraft for the Active Aeroelastic Wing (AAW) project at NASA's Dryden Flight Research Center, Edwards, California.
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This modified F/A-18A is the test aircraft for the Active Aeroelastic Wing (AAW) project at NASA's Dryden Flight Research Center, Edwards, California.
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This modified F/A-18A is the test aircraft for the Active Aeroelastic Wing (AAW) project at NASA's Dryden Flight Research Center, Edwards, California.
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NASA aircraft technician Donte Warren completes placement of the first official U.S. Centennial of Flight Commission logo on an aircraft, Dryden's Active Aeroelastic Wing (AAW) F/A-18.
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NASA aircraft technician Don Herman completes placement of the first official U.S. Centennial of Flight Commission logo on an aircraft, Dryden's Active Aeroelastic Wing (AAW) F/A-18.
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With the modified F/A-18 showcased behind him, Kevin Petersen, director of NASA Dryden Flight Research Center, addressed the audience attending the rollout ceremonies for the Active Aeroelastic Wing flight research project.
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A modified F/A-18 in a distinctive red, white and blue paint scheme was showcased during formal rollout ceremonies for the Active Aeroelastic Wing flight research program.
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NASA's Active Aeroelastic Wing F/A-18A research aircraft rolls upside down during a 360-degree aileron roll on a test mission.
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The modified F/A-18 being flown in the joint NASA/Air Force Active Aeroelastic Wing research program shows off its colors during its first checkout flight from NASA's Dryden Flight Research Center.
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NASA 853, a modified former Navy F/A-18A fighter plane, is now performing research duties in the Active Aeroelastic Wing project at NASA Dryden Flight Research Center, Edwards AFB, California.
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NASA Dryden's highly-modified Active Aeroelastic Wing F/A-18A shows off its form during a 360-degree aileron roll during a research flight.
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How differential deflection of the inboard and outboard leading-edge flaps affected the handling qualities of this modified F/A-18A was evaluated during the first check flight in the Active Aeroelastic Wing program at NASA's Dryden Flight Research Center.
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The Active Aeroelastic Wing F-18A lifts off on its first checkout flight November 15, 2002, from NASA's Dryden Flight Research Center at Edwards Air Force Base, Calif. The checkout flight initiated a two-phase NASA--Air Force flight research program that will investigate the potential of aerodynamically twisting flexible wings to improve maneuverability of high-performance aircraft at transonic and supersonic speeds.
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A modified F/A-18A undergoes wing torsion testing in the Flight Dynamics Laboratory at NASA's Dryden Flight Research Center, Edwards, California
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Structural loads testing on the Active Aeroelastic Wing F-18 in the Flight Loads Laboratory at NASA's Dryden flight Research Center, Edwards, California
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The upper wing surfaces of the Active Aeroelastic Wing F/A-18 test aircraft are covered with accelerometers and other sensors during ground vibration tests at NASA Dryden Flight Research Center.
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NASA's Active Aeroelastic Wing F/A-18 resumed flight tests in the second phase of the program at the Dryden Flight Research Center in early December 2004.
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NASA's modified Active Aeroelastic Wing F/A-18 skims over portions of the U.S. Borax mine during a recent mission from the Dryden Flight Research Center.
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NASA's Active Aeroelastic Wing F/A-18 rolls into a hard left turn during a research flight in early December 2004 from the Dryden Flight Research Center.
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NASA Dryden technicians (Dave Dennis, Freddy Green and Jeff Doughty) position a support cylinder under the right wing of the Active Aeroelastic Wing F/A-18 test aircraft prior to ground vibration tests.
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