61. Variable-geometry | Ask.com Encyclopedia In the aftermath of the cancellation of the TSR2, the British had started a project with the French for the Anglo-French Variable Geometry aircraft (AFVG). http://www.ask.com/wiki/Variable-geometry?qsrc=3044

62. Variable-sweep Wing In the aftermath of the cancellation of the TSR2, the British had started a project with the French for the Anglo-French Variable Geometry aircraft (AFVG). http://www.worldlingo.com/ma/enwiki/en/Variable-sweep_wing

Mul tili ngual Ar chi ve Po wer ed by Wor ldLi ngo Variable-sweep wing Home Multilingual Archive Index Ch oo se your la ngua ge: English Italiano Deutsch Nederlands ... Svenska var addthis_pub="anacolta"; Variable-sweep wing "Swing Wing" redirects here. For the toy, see Swing Wing (toy) A Variable-sweep wing (or swing-wing) is an airplane wing that may be swept back and then returned to its original position during flight. It allows the aircraft's planform to be modified in flight, and is therefore an example of variable geometry. Typically, a swept wing is more suitable for high speeds, while an unswept wing is suitable for lower speeds (such as when taking off and landing). A swing-wing allows a pilot to select the correct wing configuration for the plane's intended speed. The swing-wing is most useful for those aircraft that are expected to function at both low and high speed, and for this reason it has been used primarily in military aircraft The added mass and complexity required to design a plane with a swing-wing somewhat offset the benefits. As a result, swing-wings have not seen widespread adoption. Contents History of development Variable-sweep aircraft Experimental Production ... References History of development Swing-wing aircraft developed from earlier experimental aircraft that were built to study the effects of a simple swept wing. The first of these was the

63. MULTIOBJECTIVE AIRCRAFT DESIGN TO INVESTIGATE POTENTIAL GEOMETRIC Your browser may not have a PDF reader available. Google recommends visiting our text version of this document. http://pdf.aiaa.org/preview/CDReadyMATIO02_685/PV2002_5859.pdf

64. D.E.P. - Design Engineering Partners - Sectors Our designs include master planning, space geometry, aircraft, baggage and passenger handling systems listed as follows http://deppartners.com/Component/Static/Airports.asp

65. WSJ.com - Plane Geometry: Scientists Help Speed Boarding Of Aircraft Nov 2, 2005 Plane Geometry Scientists Help Speed Boarding of Aircraft. America West Saves Minutes With Reverse Pyramid ; Link to Relativity Theory http://rakaposhi.eas.asu.edu/menkes-wsj-online.htm

66. Ipacs-sim.com Geometry( aircraft/AS_LCF/AS_LCF.obj , Fuselage01 ) cd ../ Append tmgeometricobject Glass. cd Glass/ Geometry( aircraft/AS_LCF/AS_LCF.obj , Glass ) http://ipacs-sim.com/user-sites/AS_LCF.tmg

// aerofly professional // // file: AS_LCF.tmg // // - Append tmgeometricobject Fuselage cd Fuselage/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Fuselage" ) Append tmgeometricobject Fuselage01 cd Fuselage01/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Fuselage01" ) cd ../ Append tmgeometricobject Glass cd Glass/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Glass" ) cd ../ Append tmgeometricobject Seat cd Seat/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Seat" ) cd ../ Append tmgeometricobject Pilot cd Pilot/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Pilot" ) cd ../ Append tmgeometricobject Accu cd Accu/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Accu" ) cd ../ Append tmgeometricobject Receiver cd Receiver/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Receiver" ) cd ../ Append tmgeometricobject Servos cd Servos/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Servos" ) cd ../ Append tmgeometricobject Servos01 cd Servos01/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Servos01" ) cd ../ Append tmgeometricobject Engineparts1 cd Engineparts1/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Engineparts1" ) cd ../ Append tmgeometricobject Engineparts2 cd Engineparts2/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Engineparts2" ) cd ../ cd ../ Append tmgeometricobject Leftwing cd Leftwing/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftwing" ) Append tmgeometricobject Leftflap cd Leftflap/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftflap" ) cd ../ Append tmgeometricobject Leftaileron cd Leftaileron/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftaileron" ) cd ../ cd ../ Append tmgeometricobject Rightwing cd Rightwing/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightwing" ) Append tmgeometricobject Rightflap cd Rightflap/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightflap" ) cd ../ Append tmgeometricobject Rightaileron cd Rightaileron/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightaileron" ) cd ../ cd ../ Append tmgeometricobject Leftstabilizer cd Leftstabilizer/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftstabilizer" ) Append tmgeometricobject Leftelevator cd Leftelevator/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftelevator" ) cd ../ cd ../ Append tmgeometricobject Rightstabilizer cd Rightstabilizer/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightstabilizer" ) Append tmgeometricobject Rightelevator cd Rightelevator/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightelevator" ) cd ../ cd ../ Append tmgeometricobject Stabilizer cd Stabilizer/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Stabilizer" ) Append tmgeometricobject Rudder cd Rudder/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rudder" ) cd ../ cd ../ Append tmgeometricobject Propeller cd Propeller/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Propeller" ) Append tmgeometricobject Blade1 cd Blade1/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Blade1" ) cd ../ Append tmgeometricobject Blade2 cd Blade2/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Blade2" ) cd ../ cd ../ Append tmgeometricobject Leftgear cd Leftgear/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftgear" ) cd ../ Append tmgeometricobject Rightgear cd Rightgear/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightgear" ) cd ../ Append tmgeometricobject Leftskid cd Leftskid/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftfloat" ) cd ../ Append tmgeometricobject Rightskid cd Rightskid/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightfloat" ) cd ../ Append tmgeometricobject Antenna cd Antenna/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Antenna" ) cd ../ Append tmgeometricobject Leftwingstruts cd Leftwingstruts/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Leftwingstruts" ) cd ../ Append tmgeometricobject Rightwingstruts cd Rightwingstruts/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Rightwingstruts" ) cd ../ Append tmgeometricobject Frontstruts cd Frontstruts/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Frontstruts" ) cd ../ Append tmgeometricobject Backstruts cd Backstruts/ Geometry( "aircraft/AS_LCF/AS_LCF.obj", "Backstruts" ) cd ../

67. The Use Of A Master-geometry System And Computer Techniques In Technical Product by S Sich 1984 http://adsabs.harvard.edu/abs/1984Zprav...1...31S

Sign on SAO/NASA ADS Physics Abstract Service Find Similar Abstracts (with default settings below Also-Read Articles Reads History Translate This Page Title: The use of a master-geometry system and computer techniques in technical production preparation and the production of aircraft parts Authors: Publication: Zpravodaj VZLU (ISSN 0044-5355), no. 1, 1984, p. 31-35. In Czech. Publication Date: Category: Engineering (General) Origin: STI NASA/STI Keywords: AIRCRAFT PRODUCTION, COMPUTER AIDED MANUFACTURING, PRODUCTION ENGINEERING, SURFACE GEOMETRY, AIRCRAFT PARTS, DATA BASES, FIXTURES, JIGS, NUMERICAL CONTROL Bibliographic Code: Abstract Consideration is given to the use of a master-geometry system for the preparation of machine numerical-control programs for the production of gauges, forming jigs, and shaped parts of assembly fixtures in aircraft production. The digital notation of shape and dimensional information on aircraft parts, influencing the overall geometry of the aircraft, assures the objective transmission of this information through the entire sequence of production preparation stages and makes possible the production of the aforementioned parts by means of numerically controlled machines. Detailed consideration is given to the development of control programs for the production of gauges and fixtures. Bibtex entry for this abstract Preferred format for this abstract (see Preferences Find Similar Abstracts: Use: Authors Title Keywords (in text query field) Abstract Text

68. TORNADO ADV (BAe) It is a twinseat, twin-engined, variable geometry aircraft and is supersonic at all altitudes. The design authority for the Tornado is Panavia, the tri-national consortium which http://www.fas.org/man/dod-101/sys/ac/row/tornado.htm

FAS Military DOD 101 Systems ... Search TORNADO (BAe) Designed and built as a collaborative project in the UK, Germany and Italy, the Tornado is in service with all three air forces and the German Navy. Tornado is also in service in Saudi Arabia and Oman. It is a twin-seat, twin-engined, variable geometry aircraft and is supersonic at all altitudes. The design authority for the Tornado is Panavia, the tri-national consortium which comprises British Aerospace, DASA of Germany and the Italian firm Alenia. The wings of the the aircraft are high-mounted, variable, swept-back, and tapered with angular, blunt tips. There are two turbofan engines inside the body. The air intakes are diagonal and box-like alongside the fuselage forward of the wing roots. There are twin exhausts. The fuselage is solid and has a needle nose. The body thickens midsection and tapers to the tail section. There is a bubble cockpit. The tail is tall, swept-back, and has a tapered fin with a curved tip and a step in the leading edge. The flats are large, mid-mounted on the body, swept-back, and tapered with blunt tips. The Tornado GR1 strike/attack aircraft is capable of carrying a wide range of conventional stores, including the JP233 anti-airfield weapon, the ALARM anti-radar missile, and laser-guided bombs. The reconnaissance version, designated the GR1A, retains the full operational capability of the GR1. The GR1B, equipped with Sea Eagle air-to-surface missiles, undertakes the anti-surface shipping role. For self-defence, the Tornado carries Sidewinder air-to-air missiles and is fitted with twin internal 27mm cannons.

69. Parametric Design Of Aircraft Geometry Using Partial Differential Equations by M Athanasopoulos 2009 - Cited by 1 - Related articles http://portal.acm.org/citation.cfm?id=1519548.1519796

70. Variable Geometry Aircraft Passenger Stairways Variable Geometry passenger steps for serving Today's regional and commuter aircraft http://www.rhphillips.co.uk/pages/airside/variable_steps.htm

You are here: Home Page Aviation Passenger Stairways Variable Geometry Passenger Steps Menu: Welcome! About us Contact Aviation ... Site Map Specifications Sheets The specification sheets are available to view and download in Adobe Acrobat and Microsoft Word formats. Right click on icon and select save as to download chosen file. Left click to view online in chosen format. Variable Geometry Passenger Steps Covering the following models: TPS-93, SPS-93, TPS-00 You can download Adobe Acrobat Reader Here Variable Geometry Passenger Steps Variable Geometry passenger steps for serving Today's regional and commuter aircraft APPLICATION Towable aircraft passenger steps suitable for servicing most of today's commercial airliners. Various models available covering a range from 73" to 206" Broad applicability with optional canopy, lighting and side panels. Also available in self propelled and truck mounted form. Custom features available Fully adjustable height range. Easily manoeuvred via front wheel steering . Non slip stair treads . Compact and lightweight .

71. Panavia Tornado The Panavia Tornado is a Multirole aircraft developed and built in cooperation with England, Germany and Italy. It is a compact twin-engined variable-geometry aircraft http://www.aviationearth.com/aircraftdata/tornado.html

72. Parametric Design Of Aircraft Geometry Using Partial Differential File Format PDF/Adobe Acrobat Quick View http://inf.brad.ac.uk/~hugail/myPapers/AthanUgailCastro2009.pdf

73. Aviation Timeline 1930 A variable geometry aircraft is flown by Hans K rner at Breslau in Germany. 15 May Miss Ellen Church, a registered nurse from Iowa, becomes the http://www.century-of-flight.freeola.com/Aviation history/aviation timeline/1930

home aviation timeline World Aviation in 1930 January A variable geometry aircraft is flown by Hans Körner at Breslau in Germany. 15 May Miss Ellen Church, a registered nurse from Iowa, becomes the first air hostess as she welcomes 11 passengers on board a United Airlines Boeing 80A tri-motor at Oakland in California. For $125 a month the United Airlines female hostesses were involved in ground handling duties and in the air they dispensed unvarying meals consisting of fruit cocktail, fried chicken and rolls, and tea or coffee. 18 May The German airship LZ127 Graf Zeppelin makes its first crossing of the South Atlantic. 25 October The first American coast to coast air service is established by Transcontinental Western Air (TWA). Also this year...

74. Measuring Surface Geometry Of Airplane Wing By Means Of Two Methods/Orlaivio Spa (Report) by Aviation ; Transportation industry Aerial photogrammetry Research Aerodynamics Aircraft wings Airplanes Wings Surfaces (Geometry) http://www.thefreelibrary.com/Measuring surface geometry of airplane wing by mea

CacheBuster('') Printer Friendly 18,320,490 articles and books Periodicals Literature Keyword Title Author Topic Member login User name Password Remember me Join us Forgot password? Submit articles free The Free Library ... Aviation artId=227281821;usrSelf=false; Measuring surface geometry of airplane wing by means of two methods/Orlaivio sparno geometrijos matavimas dviem metodais. 1. Introduction As is widely known, the accuracy of the production of aircraft aerodynamic components is a complicated task largely influencing the aerodynamic properties of the entire aircraft. Additionally, the exploitation of the aircraft could cause some significant changes in the shape of its aerodynamic surfaces. The shape and the surface flaws of aircraft elements should therefore be controlled quite precisely (1-5 mm). Despite the influence of the shape of aerodynamic surfaces on the properties of the flight of aircraft, the geometric shape of those aerodynamic elements is quite seldom precisely controlled due to the complexity of such control. The surface (and the general shape) of the assembled aircraft can hardly be controlled by the contact measurements due to the large size of the entire aircraft; such large coordinate measuring machines can be installed at special plants and are extremely expensive. The control of dimensions by means of the arm-type coordinate measuring machines is possible, but such an approach is not always applicable too due to the quite complex surface, the need for constant repositioning of the instrument (producing additional errors), and the quite high price of the instrument. Additionally, such approaches require mechanically touching aircraft surfaces with the touch probe, and thus obtaining the large

75. The TMG-file Geometry( aircraft/AS_Deproni/AS_Deproni.obj , Engine ) Shiny = 0.00 cd ../ Append tmgeometricobject Leftgear cd Leftgear/ Geometry( aircraft/AS_Deproni/AS_Deproni.obj , Leftgear ) http://ipacs-sim.com/user-sites/the_tmg-file.htm

The tmg-file must have the same name as the obj-file , e. G. AS_Deproni.obj and AS_Deproni.tmg With the tmg-file you describe all the objects of the obj-file which belong together, you build groups The first object name is the one you will have to define in the tmd-file later on. Example: The object Fuselage contains the objects Fuselage Engine Leftgear and Rightgear The object Stabilizer consists of Stabilizer and Rudder The first and the second object of a group have no delimiter inbetween. All other objects are separated with cd ../ It is very important to use the correctly syntax , e. G. cd blank The groups are separated with lines of cd ../ A group can consist of only 1 object (e. G. Leftwheel ) and will then be separated with only cd ../ Please notice: An object of the obj-file which is not described in the tmg-file will not appear in AFP/D!! Some explanations: Geometry( "aircraft/AS_Deproni/AS_Deproni.obj", "Fuselage" ) "aircraft/AS_Deproni/AS_Deproni.obj" "Fuselage" Shiny = 1.00 Shiny = 0.00 Only for the AeroFly Professional Deluxe Below all objects of the file AS_Deproni.obj

76. Emerald Aircraft Engineering And Aerospace Technology Modern by N Lidbro 1956 http://www.emeraldinsight.com/10.1108/eb032760

77. Swing-wing - Definition Of Swing-wing By The Free Online Dictionary, Thesaurus A (Engineering / Aeronautics) of or relating to a variablegeometry aircraft. n (Engineering / Aeronautics) a. such an aircraft. b. either wing of such an aircraft http://www.thefreedictionary.com/swing-wing

78. The Efficient Parametrization Of Aircraft Geometry Dec 12, 1994 The Efficient Parametrization of Aircraft Geometry. NASA Langely Research Center has funded research to investigate the way in which the PDE http://www.amsta.leeds.ac.uk/applied/CAGD.dir/section3_4.html

Next: Computer-Aided Rapid Prototyping Up: Computer Aided Geometric and Functional Design Previous: Automatic Design for Function The Efficient Parametrization of Aircraft Geometry NASA Langely Research Center has funded research to investigate the way in which the PDE method can be used to efficiently parametrize aircraft geometry. The types of objects considered have included the a supersonic transport and nacelle/pylon configurations. Software has been developed that allows the interactive manipulation of such geometries by a user sitting at a suitable workstation. Page Created: Mon Dec 12 1994 Last Updated: 19th March 1996.

79. Gridgen Application - Geometry Repair On The C-5 Aircraft The starting point for this study is an IGES file containing geometry information for a Lockheed C5A Galaxy aircraft. The original IGES file includes 431 http://www.pointwise.com/apps/c5.shtml

Reliable People. Reliable Tools. Reliable CFD Meshing. About Us Contact Us Products Pointwise ... Support Search: Applications Applications Home Aerospace 727 T-Tail 747 Nacelle High-Lift Systems Airfoils ... X-Planes Turbomachinery Automated Meshing CFTurbo Interface Radial Blower Advanced Turbine ... Yacht Keel Automotive Solar Car Cooling Fans Motorbike Torque Converters ... Helical Intake Other Wind Energy Heart Valve Personal Micro Environment Radar Cross Section ... Bats Special Discount Top Pages Free Evaluations Free Literature Webinars Videos ... Teaching Partnership Sign Up. Keep Up. Twitter Facebook Focal Point The Connector Applications P-3C Orion Joint Strike Fighter Naval Hydro Turbine Volute ... More... C5 Transport Aircraft Geometry Repair An example of work described in the paper "Gridgen's Synergistic Implementation of CAD and Grid Geometry Modeling", from the proceedings of the 5th International Conference on Numerical Grid Generation in Computational Field Simulations, held at Mississippi State University, 01-05 Apr 96. The goal of this study is to demonstrate some of Gridgen's geometry modeling tools that are useful in repairing geometry models in preparation for gridding. Useful features of Gridgen shown in this study are: removing extraneous components from a geometry model to make the grid generation process simpler

80. Estimated Benefits Of Variable-Geometry Wing Camber Control For File Format PDF/Adobe Acrobat Quick View http://citeseerx.ist.psu.edu/viewdoc/download?doi=10.1.1.42.3212&rep=rep1&am

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