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- Boeing_X-53_Active_Aeroelastic_Wing abstract "The X-53 Active Aeroelastic Wing (AAW) development program is a completed research project that was undertaken jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works and NASA's Dryden Flight Research Center, where the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet. Active Aeroelastic Wing Technology is a technology that integrates wing aerodynamics, controls, and structure to harness and control wing aeroelastic twist at high speeds and dynamic pressures. By using multiple leading and trailing edge controls like "aerodynamic tabs", subtle amounts of aeroelastic twist can be controlled to provide large amounts of wing control power, while minimizing maneuver air loads at high wing strain conditions or aerodynamic drag at low wing strain conditions. The flight program which first proved the use of AAW technology in full scale was the X-53 Active Aeroelastic Wing program. Gerry Miller and Jan Tulinius led the development of the initial concept during wind tunnel testing in the mid 1980s under Air Force contract. The designation "X-52" was skipped in sequence to avoid confusion with the B-52 Stratofortress bomber.".
- Boeing_X-53_Active_Aeroelastic_Wing manufacturer McDonnell_Douglas.
- Boeing_X-53_Active_Aeroelastic_Wing manufacturer Northrop_Corporation.
- Boeing_X-53_Active_Aeroelastic_Wing predecessor A-18_Hornet.
- Boeing_X-53_Active_Aeroelastic_Wing type Technology_demonstration.
- Boeing_X-53_Active_Aeroelastic_Wing wikiPageExternalLink aaw.
- Boeing_X-53_Active_Aeroelastic_Wing wikiPageExternalLink i_pw.html.
- Boeing_X-53_Active_Aeroelastic_Wing wikiPageExternalLink index.html.
- Boeing_X-53_Active_Aeroelastic_Wing wikiPageID "6092100".
- Boeing_X-53_Active_Aeroelastic_Wing wikiPageRevisionID "592929183".
- Boeing_X-53_Active_Aeroelastic_Wing avionics "The leading edge flap drive system was modified at McDonnell Douglas using a new outboard actuation unit developed by Moog. AAW flight control laws were programmed into a research flight control computer modified to include an independently actuated outboard leading edge control surfaces.".
- Boeing_X-53_Active_Aeroelastic_Wing ceilingFt "50000".
- Boeing_X-53_Active_Aeroelastic_Wing crew "1".
- Boeing_X-53_Active_Aeroelastic_Wing developedFrom A-18_Hornet.
- Boeing_X-53_Active_Aeroelastic_Wing eng1Lbf "16000".
- Boeing_X-53_Active_Aeroelastic_Wing eng1Name General_Electric_F404.
- Boeing_X-53_Active_Aeroelastic_Wing eng1Number "2".
- Boeing_X-53_Active_Aeroelastic_Wing eng1Type "low-bypass turbofan engines".
- Boeing_X-53_Active_Aeroelastic_Wing firstFlight "2006-12-08".
- Boeing_X-53_Active_Aeroelastic_Wing hasPhotoCollection Boeing_X-53_Active_Aeroelastic_Wing.
- Boeing_X-53_Active_Aeroelastic_Wing heightFt "15".
- Boeing_X-53_Active_Aeroelastic_Wing heightIn "3".
- Boeing_X-53_Active_Aeroelastic_Wing manufacturer McDonnell_Douglas.
- Boeing_X-53_Active_Aeroelastic_Wing manufacturer Northrop_Corporation.
- Boeing_X-53_Active_Aeroelastic_Wing maxSpeedMph "1188".
- Boeing_X-53_Active_Aeroelastic_Wing maxTakeoffWeightLb "39000".
- Boeing_X-53_Active_Aeroelastic_Wing nationalOrigin "United States".
- Boeing_X-53_Active_Aeroelastic_Wing primaryUser NASA.
- Boeing_X-53_Active_Aeroelastic_Wing primeUnits%3F_ "kts".
- Boeing_X-53_Active_Aeroelastic_Wing seeAlso "* Aeroelasticity * Parker Variable Wing * Adaptive Compliant Wing * Aeroelastic wing on the Grumman X-29".
- Boeing_X-53_Active_Aeroelastic_Wing spanFt "38".
- Boeing_X-53_Active_Aeroelastic_Wing spanIn "5".
- Boeing_X-53_Active_Aeroelastic_Wing type Technology_demonstration.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Aircraft_configurations.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Aircraft_wing_design.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Articles_containing_video_clips.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Boeing_aircraft.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Edwards_Air_Force_Base.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Emerging_technologies.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:NASA_programs.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Twinjets.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:United_States_experimental_aircraft_2000–2009.
- Boeing_X-53_Active_Aeroelastic_Wing subject Category:Variable-geometry-wing_aircraft.
- Boeing_X-53_Active_Aeroelastic_Wing type Aircraft.
- Boeing_X-53_Active_Aeroelastic_Wing type MeanOfTransportation.
- Boeing_X-53_Active_Aeroelastic_Wing type Product.
- Boeing_X-53_Active_Aeroelastic_Wing type DesignedArtifact.
- Boeing_X-53_Active_Aeroelastic_Wing comment "The X-53 Active Aeroelastic Wing (AAW) development program is a completed research project that was undertaken jointly by the Air Force Research Laboratory (AFRL), Boeing Phantom Works and NASA's Dryden Flight Research Center, where the technology was flight tested on a modified McDonnell Douglas F/A-18 Hornet.".
- Boeing_X-53_Active_Aeroelastic_Wing label "Boeing X-53 Active Aeroelastic Wing".
- Boeing_X-53_Active_Aeroelastic_Wing label "Boeing X-53 Active Aeroelastic Wing".
- Boeing_X-53_Active_Aeroelastic_Wing label "Boeing X-53".
- Boeing_X-53_Active_Aeroelastic_Wing label "Boeing X-53".
- Boeing_X-53_Active_Aeroelastic_Wing label "X-53 (航空機)".
- Boeing_X-53_Active_Aeroelastic_Wing label "بوينغ إكس-53".
- Boeing_X-53_Active_Aeroelastic_Wing sameAs Boeing_X-53.
- Boeing_X-53_Active_Aeroelastic_Wing sameAs Boeing_X-53_Active_Aeroelastic_Wing.
- Boeing_X-53_Active_Aeroelastic_Wing sameAs Boeing_X-53_Active_Aeroelastic_Wing.
- Boeing_X-53_Active_Aeroelastic_Wing sameAs X-53_(航空機).
- Boeing_X-53_Active_Aeroelastic_Wing sameAs Boeing_X-53.
- Boeing_X-53_Active_Aeroelastic_Wing sameAs m.0fpqcn.
- Boeing_X-53_Active_Aeroelastic_Wing sameAs Q890225.
- Boeing_X-53_Active_Aeroelastic_Wing sameAs Q890225.
- Boeing_X-53_Active_Aeroelastic_Wing wasDerivedFrom Boeing_X-53_Active_Aeroelastic_Wing?oldid=592929183.
- Boeing_X-53_Active_Aeroelastic_Wing isPrimaryTopicOf Boeing_X-53_Active_Aeroelastic_Wing.