Fuselage

Results: 134



#Item
51November 04, 2014, NAGSMA – Brussels NAGSMA General Manager, Jim Edge, and NAGSMO Chairman, Erling Wang announced that the Fuselage of the second NATO AGS UAV has been completed at Northrop-Grumman’s plant at Moss Po

November 04, 2014, NAGSMA – Brussels NAGSMA General Manager, Jim Edge, and NAGSMO Chairman, Erling Wang announced that the Fuselage of the second NATO AGS UAV has been completed at Northrop-Grumman’s plant at Moss Po

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Source URL: www.nagsma.nato.int

Language: English - Date: 2014-11-14 03:28:43
52LA07.meet the members.v4.EE.indd

LA07.meet the members.v4.EE.indd

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Source URL: www.lightaircraftassociation.co.uk

Language: English - Date: 2014-09-08 08:28:14
53Kitfox Series 7 Super Sport – Pricing Information Kitfox Super Sport aircraft Firewall Back kit as noted below: (aircraft standard configuration is tail wheel) A - Kitfox Super Sport Fuselage Kit B - Wing Kit C - Landi

Kitfox Series 7 Super Sport – Pricing Information Kitfox Super Sport aircraft Firewall Back kit as noted below: (aircraft standard configuration is tail wheel) A - Kitfox Super Sport Fuselage Kit B - Wing Kit C - Landi

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Source URL: www.kitfoxaircraft.com

Language: English - Date: 2014-07-14 19:49:09
54ABOUT THE PIT ARFF TRAINING FACILITY The ARFF simulator system is computer controlled and features a 135-foot diameter propane fueled burn area with an aircraft fuselage in its center. In addition to fighting fuel spill

ABOUT THE PIT ARFF TRAINING FACILITY The ARFF simulator system is computer controlled and features a 135-foot diameter propane fueled burn area with an aircraft fuselage in its center. In addition to fighting fuel spill

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Source URL: www.flypittsburgh.com

Language: English - Date: 2014-11-18 14:48:40
55COMPARISONS OF COMPUTED AND EXPERIMENTAL PRESSURES FOR TRANSONIC FLOWS ABOUT ISOLATED WINGS AND WING-FUSELAGE CONFIGURATIONS -: . By F. R. -Bailey NASA Ames Research Center

COMPARISONS OF COMPUTED AND EXPERIMENTAL PRESSURES FOR TRANSONIC FLOWS ABOUT ISOLATED WINGS AND WING-FUSELAGE CONFIGURATIONS -: . By F. R. -Bailey NASA Ames Research Center

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Source URL: history.arc.nasa.gov

Language: English - Date: 2014-06-16 15:21:24
56USAF Wildlife Strikes by Impact Point Impact Point ECM Pods / Pylons Fuel Tanks Fuselage / Antenna / Skin

USAF Wildlife Strikes by Impact Point Impact Point ECM Pods / Pylons Fuel Tanks Fuselage / Antenna / Skin

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Source URL: www.afsec.af.mil

Language: English - Date: 2014-12-09 15:14:23
    57The aim of the STRAINMON project was to develop methodology procedures needed for the implementation of an SHM system, based on FOBG sensors and/or standard strain gauges (SGs), onto/into a CFRP fuselage stiffened panel

    The aim of the STRAINMON project was to develop methodology procedures needed for the implementation of an SHM system, based on FOBG sensors and/or standard strain gauges (SGs), onto/into a CFRP fuselage stiffened panel

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    Source URL: www.cleansky.eu

    Language: English - Date: 2014-12-12 04:54:38
    58ADHeRo Aerodynamic Design Optimization of a Helicopter Fuselage including a Rotating Rotor Head State of the art – Background The reduction of emissions is clearly one of - if not - the most challenging task of our soc

    ADHeRo Aerodynamic Design Optimization of a Helicopter Fuselage including a Rotating Rotor Head State of the art – Background The reduction of emissions is clearly one of - if not - the most challenging task of our soc

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    Source URL: www.cleansky.eu

    Language: English - Date: 2014-12-12 04:56:03
    59The aim of the STRAINMON project was to develop methodology procedures needed for the implementation of an SHM system, based on FOBG sensors and/or standard strain gauges (SGs), onto/into a CFRP fuselage stiffened panel

    The aim of the STRAINMON project was to develop methodology procedures needed for the implementation of an SHM system, based on FOBG sensors and/or standard strain gauges (SGs), onto/into a CFRP fuselage stiffened panel

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    Source URL: cleansky.eu

    Language: English - Date: 2014-12-12 04:54:38
    60ADHeRo Aerodynamic Design Optimization of a Helicopter Fuselage including a Rotating Rotor Head State of the art – Background The reduction of emissions is clearly one of - if not - the most challenging task of our soc

    ADHeRo Aerodynamic Design Optimization of a Helicopter Fuselage including a Rotating Rotor Head State of the art – Background The reduction of emissions is clearly one of - if not - the most challenging task of our soc

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    Source URL: cleansky.eu

    Language: English - Date: 2014-12-12 04:56:03