KATnet Key Aerodynamic Technologies for Aircraft Performance Improvement
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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
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