KATnet Key Aerodynamic Technologies for Aircraft Performance Improvement
|
|
|
- Rosanna Gaines
- 7 years ago
- Views:
Transcription
1 Fifth Community Aeronautical Days 2006, Vienna, Austria, June 2006 Presented by Géza Schrauf Airbus With contributions of Burkhard Gölling and Norman Wood KATnet Key Aerodynamic Technologies for Aircraft Performance Improvement 5th Community Aeronautics Days June 2006
2 The Thematic Network KATnet: Overview Project No:GTC Coordinator: Airbus Deutschland Germany Contractors: Airbus UK United Kingdom Airbus France France BAE Systems United Kingdom Alenia Aeronautica Italy DLR Germany FOI Sweden ONERA France QinetiQ United Kingdom Duration: September 2002 December 2005 DRAGNET KATnet KATnet II (will start in September 2006) 5th Community Aeronautics Days June 2006 Page 2
3 The Thematic Network KATnet: Overview 5th Community Aeronautics Days June 2006 Page 3
4 European Aeronautics: A Vision for % reduction of fuel consumption 80% reduction of NO X 50% reduction of perceived noise reduction of environmental impact of aircraft manufacturing, maintenance and disposal 5th Community Aeronautics Days June 2006 Page 4
5 Rotterdam Jet Fuel Spot Price 28 Sep ct/gal average 59ct/gal Source: US Dept. of Energy 5th Community Aeronautics Days June 2006 Page 5
6 DOC Shares for 6000 nm Mission FUEL FUEL 60 US-ct/US-gallon 180 US-ct/US-gallon 5th Community Aeronautics Days June 2006 Page 6
7 KATnet Workshops & Conferences Workshop on High Lift Aerodynamics Sep 2002 Stockholm, Sweden Workshop on High Speed Aerodynamics Sep 2003 Bath, U.K. Workshop on Flow Control Oct 2004 Poitier, France KATnet Conference Jun 2005 Bremen, Germany 5th Community Aeronautics Days June 2006 Page 7
8 TA2: High-Speed Performance KATnet/GARTEUR Workshop on High Speed Aerodynamics 3-4 September 2003 University of Bath, U.K. Contributing projects: HiReTT, Aeroshape, M-DAW GARTEUR AG 26, 28, 31, 34 National Programmes 5th Community Aeronautics Days June 2006 Page 8
9 TA2: High-Speed Design Drivers Reduce drag Reduce weight Reduce airframe costs (simpler structure with less maintenance) 5th Community Aeronautics Days June 2006 Page 9
10 Specific Range as Performance Measure Specific range SR measures performance of aircraft more efficient engine => increase bypass ratio, intercooler, lighter structure better aerodynamics => advanced materials => improve => reduce drag TSFC = thrust specific fuel consumption = weight of fuel consumed during time increment / ( time increment * thrust ) 5th Community Aeronautics Days June 2006 Page 10
11 Drag Breakdown of Transport Aircraft in Cruise 5th Community Aeronautics Days June 2006 Page 11
12 Cruise Drag Reduction Reduce friction drag Delay lam./turb. transition Natural laminar flow (shaping) Hybrid laminar flow control (suction) Active flow control (wave cancellation) Reduce lift-dependent drag Elliptic lift distribution has minimal vortex drag Use advanced materials and optimise installation to shift the overall optimum towards an elliptic lift distribution (reduces drag and weight) 5th Community Aeronautics Days June 2006 Page 12
13 Cruise Drag Reduction Reduce lift-dependent drag (cont.) Novel configurations 5th Community Aeronautics Days June 2006 Page 13
14 Other Cruise Technologies Reduce design constraints using new materials Shape optimisation Wing tip devices Adaptive wing devices Multi-functional control surfaces Mini trailing edge devices Load control Gust / manoeuvre load alleviation 5th Community Aeronautics Days June 2006 Page 14
15 TA1: Low-Speed Performance KATnet/GARTEUR High Lift Workshop September 2002 Stockholm, Sweden Contributing projects: GARTEUR AG 25, 36 EUROLIFT, Helix, EPISTLE, HiAer National Programmes 5th Community Aeronautics Days June 2006 Page 15
16 TA1: High-Lift Design Drivers Aerodynamics: improve high-lift performance maximum lift low take-off drag improve ice accretion prediction capability Systems: simplify high lift system low system complexity with acceptable handling quality Structure: reduce weight DOC: reduce airframe costs simpler structure with less maintenance Airport capacity: increase landing and take-off rates wake vortex separation Aeroacoustics: reduce community noise target: leave noise foot print in airport area reduce noise of high-lift components and landing gear 5th Community Aeronautics Days June 2006 Page 16
17 TA3: Flow Control Technologies KATnet Flow Control Workshop October 2004 Poitiers, France Contributing projects: AWIATOR, ALTTA, HYLTEC, AEROMEMS I & II, HELIX, M-DAW ERCOFTAC SIG, National Flow Control Programmes 5th Community Aeronautics Days June 2006 Page 17
18 TA3: Research Needs for Drag Reduction Drag reduction by laminar flow - simplified suction systems U WAVEPACKET AMPLIFICATION CANCELLATION - in-flight skin friction sensors Sensor Actuator Sensor - anti-contamination surface coatings Exciter CONTROL SYSTEM -active control of Tollmien-Schlichting instabilities / microroughness Drag reduction by turbulent flow manipulation - dimples, riblets - compliant surfaces - active manipulation of near wall turbulent flow structures by MEMS - low energy plasma technologies 5th Community Aeronautics Days June 2006 Page 18
19 TA3: Research Needs for Separation Control Research needs for separation control - air-jet vortex generators steady, unsteady, positive & zero mass flux - tangential and pulsed blowing 5th Community Aeronautics Days June 2006 Page 19
20 KATnet Baseline Configurations Enable universities to evaluate their technologies by providing baseline configurations (short range, long range, supersonic) including - top-level aircraft requirements - basic aerodynamic data - estimated weight break down - simplified performance spread sheet 5th Community Aeronautics Days June 2006 Page 20
21 KATnet Website: KATnet website will be maintained and updated in KATnet II 5th Community Aeronautics Days June 2006 Page 21
22 Outlook to KATnet II KATnet II structure 5th Community Aeronautics Days June 2006 Page 22
23 This document and all information contained herein is the sole property of AIRBUS DEUTSCHLAND GmbH. No intellectual property rights are granted by the delivery of this document or the disclosure of its content. This document shall not be reproduced or disclosed to a third party without the express written consent of AIRBUS DEUTSCHLAND GmbH. This document and its content shall not be used for any purpose other than that for which it is supplied. The statements made herein do not constitute an offer. They are based on the mentioned assumptions and are expressed in good faith. Where the supporting grounds for these statements are not shown, AIRBUS DEUTSCHLAND GmbH will be pleased to explain the basis thereof. 5th Community Aeronautics Days June 2006 Page 23
Computational Fluid Dynamics
Aerodynamics Computational Fluid Dynamics Industrial Use of High Fidelity Numerical Simulation of Flow about Aircraft Presented by Dr. Klaus Becker / Aerodynamic Strategies Contents Aerodynamic Vision
Smart Fixed Wing Aircraft Integrated Technology Demonstrator (SFWA-ITD): New Wing Concepts
Aerodays 2011 conference CleanSky Scenarios for 2020: Conceptual Aircraft Smart Fixed Wing Aircraft Integrated Technology Demonstrator (SFWA-ITD): New Wing Concepts Madrid, 30. March 01. April 2010 J.
The Natural Laminar Flow Ground Based Demonstrator
The Natural Laminar Flow Ground Based Demonstrator The Ground Based Demonstrator (GBD) project was a collaboration between Airbus and GKN funded by European Clean Sky 1. The GBD is a full scale partial
Circulation Control NASA activities
National Aeronautics and Space Administration Circulation Control NASA activities Dr. Gregory S. Jones Dr. William E. Millholen II Research Engineers NASA Langley Research Center Active High Lift and Impact
Programme Discussions Wissenschaftstag Braunschweig 2015 Laminarität für zukünftige Verkehrsflugzeuge
Programme Discussions Wissenschaftstag Braunschweig 2015 Kevin Nicholls, EIVW Prepared by Heinz Hansen TOP-LDA Leader, ETEA Presented by Bernhard Schlipf, ESCRWG Laminarität für zukünftige Verkehrsflugzeuge
Best Practices for Fuel Economy
AACO ICAO Operational Technical Forum Measures / Beirut, Workshop 19th of / November Montreal, 20/21 2005 September 2006 Presented by: Olivier HUSSE Senior Performance Engineer Best Practices for Fuel
Faculty of Aerospace Engineering
Delft University of Technology Dr. ir. Roeland De Breuker and Dr. Arvind Rao 20-3-2013 Delft University of Technology Challenge the future Delft University of Technology General Information Founded in
OVERVIEW ON DRAG REDUCTION TECHNOLOGIES FOR CIVIL TRANSPORT AIRCRAFT
European Congress on Computational Methods in Applied Sciences and Engineering ECCOMAS 2004 P. Neittaanmäki, T. Rossi, S. Korotov, E. Oñate, J. Périaux, and D. Knörzer (eds.) Jyväskylä, 24 28 July 2004
APP Aircraft Performance Program Demo Notes Using Cessna 172 as an Example
APP Aircraft Performance Program Demo Notes Using Cessna 172 as an Example Prepared by DARcorporation 1. Program Layout & Organization APP Consists of 8 Modules, 5 Input Modules and 2 Calculation Modules.
CROR Noise Generation Mechanism #3: Installation Effects (& Quadrupole Noise)
CROR Noise Generation Mechanism #3: Installation Effects (& Quadrupole Noise) Arne Stuermer & Jianping Yin Institute of Aerodynamics & Flow Technology DLR Braunschweig Germany 14th CEAS-ASC Workshop October
Industrial Application of CFD in Airbus
STAR Konferenz Deutschland 9.-10. November 2009 November 2009 Dr.-Ing. Andreas Wick Environmental Control Systems CFD Focal Point Airbus Operations GmbH Industrial Application of CFD in Airbus An Air Systems
Aircraft performance monitoring
Regional Seminar Aircraft performance monitoring Presented by Steve BARKER / Senior Performance Engineer Contents 1 2 3 4 5 6 7 What is aircraft performance monitoring? Performance monitoring principle
INFO DAYS FP7 2nd Call
Rzeszow, 2008.03.11-12 Integrated Design Flight Mechanics performance optimization Andrzej MAJKA Integrated design of personal aircrafts fleet (multidisciplinary problem) Problems: Problem formulation
AIRBUS CORPORATE ANSWER TO DISSEMINATE ENVIRONMENTAL MANAGEMENT SYSTEM. Environmental requirements for suppliers and management of the supply chain
ACADEMY AIRBUS CORPORATE ANSWER TO DISSEMINATE ENVIRONMENTAL MANAGEMENT SYSTEM ECO-EFFICIENCY AND SUSTAINABILITY - G7 - ISSUE 1 Environmental requirements for suppliers and management of the supply chain
Wing Design: Major Decisions. Wing Area / Wing Loading Span / Aspect Ratio Planform Shape Airfoils Flaps and Other High Lift Devices Twist
Wing Design: Major Decisions Wing Area / Wing Loading Span / Aspect Ratio Planform Shape Airfoils Flaps and Other High Lift Devices Twist Wing Design Parameters First Level Span Area Thickness Detail Design
Green Regional Aircraft ITD
Green Regional Aircraft ITD Prepared by Rocco Pinto (AleniaAermacchi) Clean Sky Call 13 Info Day Paris, 6 th July 2012 Clean Sky - General Technical Organization Vehicle ITD Eco-design For Airframe and
TsAGI EU Scientific Cooperation National Contact Point Aeronautics
CENTRAL AEROHUYDRODYNAMIC INSTITUTE NAMED AFTER PROF. N.E. ZHUKOVSKY TsAGI EU Scientific Cooperation National Contact Point Aeronautics Central Aerohydrodynamic Institute (TsAGI) named after prof. N.E.
Practice Problems on Boundary Layers. Answer(s): D = 107 N D = 152 N. C. Wassgren, Purdue University Page 1 of 17 Last Updated: 2010 Nov 22
BL_01 A thin flat plate 55 by 110 cm is immersed in a 6 m/s stream of SAE 10 oil at 20 C. Compute the total skin friction drag if the stream is parallel to (a) the long side and (b) the short side. D =
Effective Configuration Management through Standardisation
10. April 2008 Presented by Matthias HOFMANN Configuration Management Consultant AIRBUS CIMPA Frank MÜLLER Head Of Configuration Management EADS Defence Electronics Effective Configuration Management through
How To Reduce The Risk Of Innovation In Bombardier Aerospace
Bombardier Aerospace: Reducing the risk of Innovation A presentation to the McMaster University Advanced Manufacturing Summit November 2014 aunch dates Bombardier is committed to innovation through product
CFD analysis for road vehicles - case study
CFD analysis for road vehicles - case study Dan BARBUT*,1, Eugen Mihai NEGRUS 1 *Corresponding author *,1 POLITEHNICA University of Bucharest, Faculty of Transport, Splaiul Independentei 313, 060042, Bucharest,
PhD Program in Aerospace Engineering
PhD Program in Aerospace Engineering INTEGRATED PROJECT IN AEROSPACE VEHICLES AND SYSTEMS 1. Summary of the motivation for the Project Aerospace Engineering is a synthesis of advanced technologies: aerodynamics,
High-Lift Systems. High Lift Systems -- Introduction. Flap Geometry. Outline of this Chapter
High-Lift Systems Outline of this Chapter The chapter is divided into four sections. The introduction describes the motivation for high lift systems, and the basic concepts underlying flap and slat systems.
Aeronautical Testing Service, Inc. 18820 59th DR NE Arlington, WA 98223 USA. CFD and Wind Tunnel Testing: Complimentary Methods for Aircraft Design
Aeronautical Testing Service, Inc. 18820 59th DR NE Arlington, WA 98223 USA CFD and Wind Tunnel Testing: Complimentary Methods for Aircraft Design Background Introduction ATS Company Background New and
Meeting Room Booking System Allan MacDougall. Room Booking System at Airbus, Filton.
Meeting Room Booking System Allan MacDougall Room Booking System at Airbus, Filton. Content Company Overview Room booking system summary Business Issues Key Benefit Summary of overall benefits 2015 Airbus
Wind Tunnels and the ATI Technology Infrastructure Strategy
Wind Tunnels and the ATI Technology Infrastructure Strategy Dr. Simon Prince Royal Aeronautical Society Conference on Wind Tunnel Capabilities. 19 th October 1015. Overview 1. The Role of Wind Tunnels:
Current Status and Challenges in CFD at the DLR Institute of Aerodynamics and Flow Technology
Current Status and Challenges in CFD at the DLR Institute of Aerodynamics and Flow Technology N. Kroll, C.-C. Rossow DLR, Institute of Aerodynamics and Flow Technology DLR Institute of Aerodynamics and
CAMRAD II COMPREHENSIVE ANALYTICAL MODEL OF ROTORCRAFT AERODYNAMICS AND DYNAMICS
CAMRAD II COMPREHENSIVE ANALYTICAL MODEL OF ROTORCRAFT AERODYNAMICS AND DYNAMICS 1 CAMRAD II IS AN AEROMECHANICAL ANALYSIS OF HELICOPTERS AND ROTORCRAFT INCORPORATING ADVANCED TECHNOLOGY multibody dynamics
RECYCLING OLD WEIGHT ASSESSMENT METHODS AND GIVING THEM NEW LIFE IN AIRCRAFT CONCEPTUAL DESIGN
28 TH INTERNATIONAL CONGRESS OF THE AERONAUTICAL SCIENCES Abstract RECYCLING OLD WEIGHT ASSESSMENT METHODS AND GIVING THEM NEW LIFE IN AIRCRAFT CONCEPTUAL DESIGN Aircraft conceptual design is an iterative
Design and Analysis of Spiroid Winglet
Design and Analysis of Spiroid Winglet W.GiftonKoil Raj 1, T.AmalSeba Thomas 2 PG Scholar, Dept of Aeronautical Engineering, Hindustan Institute of Technology and Science, Chennai, India 1 Assistant Professor,
Aerodynamic Design Optimization Discussion Group Case 4: Single- and multi-point optimization problems based on the CRM wing
Aerodynamic Design Optimization Discussion Group Case 4: Single- and multi-point optimization problems based on the CRM wing Lana Osusky, Howard Buckley, and David W. Zingg University of Toronto Institute
FISS Full In Service Support
Market Development Services Design & Edition I September 2014 I EN FISS Full In Service Support EADS CONSTRUCCIONES AERONAUTICAS, S.A.U. (EADS CASA) Avenida de Aragón, 404-28022 Madrid, SPAIN Phone: +34
Airplane wing test stand for simulating the airstream. Airbus Deutschland GmbH
Airplane wing test stand for simulating the airstream Airbus Deutschland GmbH 2 1 Airplane wing test stand for simulating the airstream Hänchen ist standard In test stands at Airbus in Bremen, Hänchen
General aviation & Business System Level Applications and Requirements Electrical Technologies for the Aviation of the Future Europe-Japan Symposium
General aviation & Business System Level Applications and Requirements Electrical Technologies for the Aviation of the Future Europe-Japan Symposium 26 March 2015 2015 MITSUBISHI HEAVY INDUSTRIES, LTD.
Contents AVIATION ENVIRONMENT ISSUES NOISE SONIC BOOM EMISSION ALTERNATIVE AVIATION FUEL. 14.10.2012 JAXA Aeronautics Symposium in Nagoya
CENTRAL AEROHYDRODYNAMIC INSTITUTE CENTRAL AEROHYDRODYNAMIC NAMED AFTER PROFESSOR N.E. ZHUKOVSKY INSTITUTE NAMED AFTER PROFESSOR N.E. ZHUKOVSKY TSAGI RESEARCH CAPABILITIES TO ADDRESS AVIATION ENVIRONMENTAL
MDO of Forward Swept Wings
MDO of Forward Swept Wings KATnet II Workshop, 28-29 January 2008, Braunschweig Martin Hepperle DLR Institute of Aerodynamics and Flow Technology, Braunschweig Folie 1 Martin Hepperle Institute of Aerodynamics
Flap Optimization for Take-off and Landing
Proceedings of the 10th Brazilian Congress of Thermal Sciences and Engineering -- ENCIT 2004 Braz. Soc. of Mechanical Sciences and Engineering -- ABCM, Rio de Janeiro, Brazil, Nov. 29 -- Dec. 03, 2004
APPENDIX 3-B Airplane Upset Recovery Briefing. Briefing. Figure 3-B.1
APPENDIX 3-B Airplane Upset Recovery Briefing Industry Solutions for Large Swept-Wing Turbofan Airplanes Typically Seating More Than 100 Passengers Briefing Figure 3-B.1 Revision 1_August 2004 Airplane
Computational Modeling of Wind Turbines in OpenFOAM
Computational Modeling of Wind Turbines in OpenFOAM Hamid Rahimi hamid.rahimi@uni-oldenburg.de ForWind - Center for Wind Energy Research Institute of Physics, University of Oldenburg, Germany Outline Computational
Coupled CFD and Vortex Methods for Modelling Hydro- and Aerodynamics of Tidal Current Turbines and On- and Offshore Wind Turbines
Coupled CFD and Vortex Methods for Modelling Hydro- and Aerodynamics of Tidal Current Turbines and On- and Offshore Wind Turbines SIMPACK User Meeting 2014 Augsburg, Germany October 9 th, 2014 Dipl.-Ing.
CFD Analysis on Airfoil at High Angles of Attack
CFD Analysis on Airfoil at High Angles of Attack Dr.P.PrabhakaraRao¹ & Sri Sampath.V² Department of Mechanical Engineering,Kakatiya Institute of Technology& Science Warangal-506015 1 chantifft@rediffmail.com,
ATR. freighter versions
ATR freighter versions ATR freighter versions ATR AND CARGO MARKET ATR Freighter Fleet In service (Dec 21) 31 4 5 3 5 2 2 Photo: Ron Baak, Netherlands. First ATR 72 Freighter delivery took place in July
Aerion and Airbus Group, Inc. Announce New Agreement, Expanded Collaboration
P R E S S I N F O R M A T I O N Aerion and Airbus Group, Inc. Announce New Agreement, Expanded Collaboration More North American-based Airbus Group, Inc. resources made available to bring the supersonic
Flight path optimization for an airplane
Flight path optimization for an airplane Dorothée Merle Master's Thesis Submission date: June 2011 Supervisor: Per-Åge Krogstad, EPT Norwegian University of Science and Technology Department of Energy
High-Speed Demonstration of Natural Laminar Flow Wing & Load Control for Future Regional Aircraft through innovative Wind Tunnel Model
High-Speed Demonstration of Natural Laminar Flow Wing & Load Control for Future Regional Aircraft through innovative Wind Tunnel Model Project organization The project tackles the CfP JTI-CS-2012-1-GRA-02-019
Toward Zero Sonic-Boom and High Efficiency. Supersonic Bi-Directional Flying Wing
AIAA Paper 2010-1013 Toward Zero Sonic-Boom and High Efficiency Supersonic Flight: A Novel Concept of Supersonic Bi-Directional Flying Wing Gecheng Zha, Hongsik Im, Daniel Espinal University of Miami Dept.
TYPE CERTIFICATE DATA SHEET Nº EA-2011T03 Type Certificate Holder: COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Via Tasso, 478 80127 - Napoli Italy
TYPE CERTIFICATE DATA SHEET Nº EA-2011T03 Type Certificate Holder: COSTRUZIONI AERONAUTICHE TECNAM S.r.l. Via Tasso, 478 80127 - Napoli Italy EA-2011T03-02 Sheet 01 TECNAM P2006T 04 May 2012 This data
Flight Operations Briefing Notes
Flight Operations Briefing Notes I Introduction Encountering wake turbulence in flight can be a surprising experience, both for crews and passengers. Wake turbulence occurs suddenly, and is usually accompanied
T E A C H E R S N O T E S
T E A C H E R S N O T E S Focus: Students explore air and its properties. They will also learn about the connection between air pressure and weather, forces that can be used for flight, how these forces
MARCH 2011 WISE. World In-Service Experience
MARCH 2011 WISE Content WISE Family Introduction WISE Knowledge Base WISE Component Performance & Recommendations WISE Main Adopted Solutions & Tips Conclusion Page 2 Introduction A source of information
Design and Structural Analysis of the Ribs and Spars of Swept Back Wing
Design and Structural Analysis of the Ribs and Spars of Swept Back Wing Mohamed Hamdan A 1, Nithiyakalyani S 2 1,2 Assistant Professor, Aeronautical Engineering & Srinivasan Engineering College, Perambalur,
Reach for the skies. The Aerospace Growth Partnership. Industry and government working together to secure the future for UK aerospace
Reach for the skies The Aerospace Growth Partnership Industry and government working together to secure the future for UK aerospace Maintaining our leadership as an aerospace nation The UK has a great
ESTIMATING R/C MODEL AERODYNAMICS AND PERFORMANCE
ESTIMATING R/C MODEL AERODYNAMICS AND PERFORMANCE Adapted from Dr. Leland M. Nicolai s Write-up (Technical Fellow, Lockheed Martin Aeronautical Company) by Dr. Murat Vural (Illinois Institute of Technology)
Comfort without compromise
Zuzana Hrnkova Head of Aircraft Interiors Marketing Comfort without compromise Every inch counts How can an airframe manufacturer influence cabin comfort and efficiency? Does an inch really matter? Efficient
Application of CFD Simulation in the Design of a Parabolic Winglet on NACA 2412
, July 2-4, 2014, London, U.K. Application of CFD Simulation in the Design of a Parabolic Winglet on NACA 2412 Arvind Prabhakar, Ayush Ohri Abstract Winglets are angled extensions or vertical projections
Airbus PLM A350 Manufacturing Engineering strategy
Jean-Bernard Hentz PLM R&T Airbus PLM A350 Manufacturing Engineering strategy Content 1 1 AIRBUS today 2 2 AIRBUS PLM Strategy for manufacturing 3 Some ideas for advanced research 4 Conclusion a world
A. Hyll and V. Horák * Department of Mechanical Engineering, Faculty of Military Technology, University of Defence, Brno, Czech Republic
AiMT Advances in Military Technology Vol. 8, No. 1, June 2013 Aerodynamic Characteristics of Multi-Element Iced Airfoil CFD Simulation A. Hyll and V. Horák * Department of Mechanical Engineering, Faculty
4 OPERATING COSTS AND EFFICIENCY OF CARGO AIRCRAFT
4 OPERATING COSTS AND EFFICIENCY OF CARGO AIRCRAFT The cost for air cargo operations is relatively complex and fluid because of four factors: Aircraft technology, Route characteristics, Structure of operations,
Airbus Procurement Organisation & Major Suppliers
Airbus Presentation Airbus Airbus Organisation & Major Suppliers Airbus Presentation Organisational Structure Airbus & Airbus Group Strategy & Services Commodities Aerostructure Airbus Group General *
Commandes de vol électriques Airbus: une approche globale de la sûreté de fonctionnement
Systèmes & Logiciels pour les NTIC dans le Transport 18 mai 2006 Presented by Pascal TRAVERSE Prepared with Isabelle LACAZE & Jean SOUYRIS Commandes de vol électriques Airbus: une approche globale de la
Laminar Flow Control Back to the Future?
38th Fluid Dynamics Conference and Exhibit 3-6 June 8, Seattle, Washington AIAA 8-3738 Laminar Flow Control Back to the Future? John E. Green 1 Aircraft Research Association Ltd., Bedford UK, MK41
LOCKHEED GEORGIA LOWSPEED WIND TUNNEL HONDA CIVIC HATCHBACK AIRTAB(R) MODIFICATION RESULTS
LOCKHEED GEORGIA LOWSPEED WIND TUNNEL HONDA CIVIC HATCHBACK AIRTAB(R) MODIFICATION RESULTS Executive Summary: This report shows conclusively that the Airtab product reduced aerodynamic drag forces at the
Regulations for Airport of Zurich Noise Fund (AZNF)
Regulations for Airport of Zurich Noise Fund (AZNF) Version 01/2016 Zurich-Airport, March 04, 2016 Flughafen Zürich AG P.O. Box, CH-8058 Zurich-Airport www.zurich-airport.com 1. Concept of the AZNF 3 2.
CFD ANALYSIS OF RAE 2822 SUPERCRITICAL AIRFOIL AT TRANSONIC MACH SPEEDS
CFD ANALYSIS OF RAE 2822 SUPERCRITICAL AIRFOIL AT TRANSONIC MACH SPEEDS K.Harish Kumar 1, CH.Kiran Kumar 2, T.Naveen Kumar 3 1 M.Tech Thermal Engineering, Sanketika Institute of Technology & Management,
Highly Optimizable Laminar Flow Control Devices
Highly Optimizable Laminar Flow Control Devices Johan Valentin Krier 1, Triyantono Sucipto 1 1 IBK-Ingenieurbuero, Rehdorfer Str. 4, D-90431 Nuremberg, Germany E-mail: Johann.Krier@ibk-tech.de, Triyantono.Sucipto@ibk-tech.de
Experimental investigation of golf driver club head drag reduction through the use of aerodynamic features on the driver crown
Available online at www.sciencedirect.com Procedia Engineering 00 (2013) 000 000 www.elsevier.com/locate/procedia The 2014 conference of the International Sports Engineering Association Experimental investigation
NASA STI Program... in Profile
NASA/TM 2015-218860 Funding and Strategic Alignment Guidance for Infusing Small Business Innovation Research Technology Into NASA Programs Associated With the Aeronautics Research Mission Directorate Hung
Lift and Drag on an Airfoil ME 123: Mechanical Engineering Laboratory II: Fluids
Lift and Drag on an Airfoil ME 123: Mechanical Engineering Laboratory II: Fluids Dr. J. M. Meyers Dr. D. G. Fletcher Dr. Y. Dubief 1. Introduction In this lab the characteristics of airfoil lift, drag,
Content must not be changed in any way or reproduced in any format or medium without the formal permission of the copyright holder(s)
nn Ferguson, K., and Thomson, D. (2015) Performance comparison between a conventional helicopter and compound helicopter configurations. Proceedings of the Institution of Mechanical Engineers, Part G:
Forces on the Rocket. Rocket Dynamics. Equation of Motion: F = Ma
Rocket Dynamics orces on the Rockets - Drag Rocket Stability Rocket Equation Specific Impulse Rocket otors Thrust orces on the Rocket Equation of otion: = a orces at through the Center of ass Center of
Technologies for Re-entry Vehicles. SHEFEX and REX FreeFlyer, DLR s Re-Entry Program. Hendrik Weihs. Folie 1. Vortrag > Autor > Dokumentname > Datum
Technologies for Re-entry Vehicles SHEFEX and REX FreeFlyer, DLR s Re-Entry Program Hendrik Weihs Folie 1 DLR`s Re-Entry Program, Why? Re-entry or return technology respectively, is a strategic key competence
Light Aircraft Design
New: Sport Pilot (LSA) The Light Aircraft Design Computer Program Package - based on MS-Excelapplication was now extented with the new Sport Pilots (LSA) loads module, which includes compliance for the
HPC@Airbus. ISC- HPC I/O in the Datacentre. I/O in an Industrial Scientific Computing Environment. Gerd Büttner. July 2015
ISC- HPC I/O in the Datacentre Gerd Büttner HPC@Airbus I/O in an Industrial Scientific Computing Environment Airbus is a global aircraft manufacturer 55,000 40billion 9yrs 400 Passion - Our global workforce
Samlesbury site & lean manufacturing. Frank Hayden Integrated Operations Director
Samlesbury site & lean manufacturing Frank Hayden Integrated Operations Director Samlesbury Site 4,500 people, Airframe design and manufacturing, In-service aircraft support Track record of international
Opus: University of Bath Online Publication Store http://opus.bath.ac.uk/
Wilson, P. (2015) Electric aircraft the future of aviation or just wishful thinking? The Conversation. Link to official URL (if available): Opus: University of Bath Online Publication Store http://opus.bath.ac.uk/
AEROSPACE ENGINEERING SERIES, GS-0861
TS-124 May 1993 General Schedule Position Classification Flysheet AEROSPACE ENGINEERING SERIES, GS-0861 Theodore Roosevelt Building 1900 E Street, NW Washington, DC 20415-8330 Classification Programs Division
Design and Development of Transport Aircraft Systems
Richard Smyth Design and Development of Transport Aircraft Systems RAeS, DGLR, VDI, HAW Hamburg Collaborative Engineering in Systems Development Contents Objectives and Drivers The Systems Development
In-flight Evaluation of Avionic Systems
In-flight Evaluation of Avionic Systems Henk Jentink National Aerospace Laboratory NLR, Flight Test Seminar, 6 April 2011, Hamburg Nationaal Lucht- en Ruimtevaartlaboratorium National Aerospace Laboratory
Overview of consolidation centres for urban and specialist use
Overview of consolidation centres for urban and specialist use Allan Woodburn University of Westminster 1 Structure of presentation General background and key questions Terminology and functions Range
AE 430 - Stability and Control of Aerospace Vehicles
AE 430 - Stability and Control of Aerospace Vehicles Atmospheric Flight Mechanics 1 Atmospheric Flight Mechanics Performance Performance characteristics (range, endurance, rate of climb, takeoff and landing
Fundamental Aeronautics Student Competition High School Division (Advanced Curriculum): 2008-2009 Academic Year
Fundamental Aeronautics Student Competition High School Division (Advanced Curriculum): 2008-2009 Academic Year THE Lazarus T1 Arcadia High School 180 Campus Drive Arcadia, CA 91006 2008-2009 School Year
UAS Perspective and Research Initiatives in Alenia Aeronautica
UAS Perspective and Research Initiatives in Alenia Aeronautica Il materiale contenuto in questa presentazione (Materiale) è di proprietà di Alenia Aeronautica S.p.A. (Alenia). È vietato qualsiasi utilizzo
CC RH A STUDY ON THE OPTIMIZATION OF JET ENGINES FOR COMBAT AIRCRAFTS. C. SSnchez Tarifa* E. Mera Diaz**
A STUDY ON THE OPTIMIZATION OF JET ENGINES FOR COMBAT AIRCRAFTS C. SSnchez Tarifa* E. Mera Diaz** Abstract In the paper the optimization of jet engines for combat aircrafts is discussed. This optimization
IT SOLUTIONS. Market Development Services Design & Edition I September 2014 I EN
Market Development Services Design & Edition I September 2014 I EN IT SOLUTIONS EADS CONSTRUCCIONES AERONAUTICAS, S.A.U. (EADS CASA) Avenida de Aragón, 404-28022 Madrid, SPAIN Phone: +34 91 585 7387/5561
pocket product guide
pocket product guide About us Becker rudder profiles Established in 1946 and located in Hamburg, Germany Becker Marine Systems is a leading supplier of high performance rudders and manoeuvring systems
How To Make A Safe Landing
Towards understanding of wake vortex evolution during approach and landing with and w/o plate lines F. Holzäpfel 1, A. Stephan 1, T. Misaka 1,2, S. Körner 1 1 Institut für Physik der Atmosphäre, DLR, Oberpfaffenhofen,
The company Premium AEROTEC
The company Premium AEROTEC was founded as an independent company on 1 January 2009 and is a wholly owned subsidiary of EADS N.V. EADS Augsburg plant and Airbus Nordenham and Varel plants have been integrated
Joints - Rolls-Royce Perspective
Joints - Rolls-Royce Perspective Dr John Schofield / Dr Jeff Green Joints Workshop April 2009. 2009 Rolls-Royce plc The information in this document is the property of Rolls-Royce plc and may not be copied
13th January 2015 John Leahy Chief Operating Officer, Customers
John Leahy Chief Operating Officer, Customers 2014 Airbus headlines 1,456 net orders (1,503 in 2013) 6,386 aircraft backlog (5,559 end 2013) A landmark year - Airbus sales total grows to 15,271 629 aircraft
Introductory FLUENT Training
Chapter 10 Transient Flow Modeling Introductory FLUENT Training www.ptecgroup.ir 10-1 Motivation Nearly all flows in nature are transient! Steady-state assumption is possible if we: Ignore transient fluctuations
New Perspectives in Aeronautics Research for the UK The Aerospace Technology Institute. Dr Simon Weeks CTO, ATI
New Perspectives in Aeronautics Research for the UK The Aerospace Technology Institute Dr Simon Weeks CTO, ATI The Aerospace Technology Institute Overview An independent institute established as a collaboration
Platform Technology for Computational Fluid Dynamics Supporting Design of System Products
Hitachi Review Vol. 61 (2012), No. 6 244 Platform Technology for Computational Fluid Dynamics Supporting Design of System Products from Power Plants and Industrial Machinery to Home Appliances Shigehisa
An insight into some innovative cycles for aircraft propulsion
731 An insight into some innovative cycles for aircraft propulsion G Corchero 1, J L Montañés 1, D Pascovici 2, and S Ogaji 2 1 Universidad Politécnica de Madrid (UPM), E. T. S. Ingenieros Aeronáuticos,
Simulation of Fluid-Structure Interactions in Aeronautical Applications
Simulation of Fluid-Structure Interactions in Aeronautical Applications Martin Kuntz Jorge Carregal Ferreira ANSYS Germany D-83624 Otterfing Martin.Kuntz@ansys.com December 2003 3 rd FENET Annual Industry