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Geometry Aircraft: more books (55)

Reliability Analysis of the 4.5 Roller Bearing by Cole Miller, 2003
Test at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing (Technical report) by M. D Dobson, 1968
Software Support Cost Estimating Models: A Comparative Study of Model Content and Parameter Sensitivity by Kevin L. Brummert, Philip Mischler, 1998
Users manual for the improved NASA Lewis ice accretion code LEWICE 1.6 (SuDoc NAS 1.26:198355) by William B. Wright, 1995
Aerodynamic shape optimization of a HSCT type configuration with improved surface definition progress report for the period ended June 30, 1994 (SuDoc NAS 1.26:197011) by A. M. Thomas, 1994
Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle (SuDoc NAS 1.26:195460) by Ganesh Raman, 1996
Ultra-high bypass ratio jet noise (SuDoc NAS 1.26:195394) by John, K. C. Low, 1994
Computational methods for global local analysis (NASA technical memorandum) by Jonathan B Ransom, 1992
Geometric modeling for computer aided design summary of research (final report) for the period ended June 30, 1995 (SuDoc NAS 1.26:198828) by James L. Schwing, 1995
Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case (SuDoc NAS 1.15:106686) by Joseph F. Baumeister, 1994
Sequential Transformation of Carbon Tetrachloride, Perchloroethylene, and 1,1, 1-Trichloroethane Using Methanogenic and Methanotrophic Conditions by Sarah J. Christ, 1997
Computer-aided light sheet flow visualization using photogrammetry (SuDoc NAS 1.60:3416) by Kathryn Stacy, 1994
HOMAR:a computer code for generating homotopic grids using algebraic relations users' manual (SuDoc NAS 1.26:4243) by Anutosh Moitra, 1989

lists with details

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
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

Extractions: var addthis_pub="anacolta"; "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. 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
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
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
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
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

Extractions: // 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 ../
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

Extractions: 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 Use: Authors Title Keywords (in text query field) Abstract Text
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

Extractions: 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.
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
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

Extractions: You are here: Home Page Aviation Passenger Stairways Variable Geometry Passenger Steps 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. Covering the following models: TPS-93, SPS-93, TPS-00 You can download Adobe Acrobat Reader Here Variable Geometry Passenger Steps 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 .
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
Parametric Design Of Aircraft Geometry Using Partial Differential
File Format PDF/Adobe Acrobat Quick View
http://inf.brad.ac.uk/~hugail/myPapers/AthanUgailCastro2009.pdf
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

Extractions: 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
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

Extractions: 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
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

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

Extractions: Previous: Automatic Design for Function 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
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

Extractions: 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 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... 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
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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