The Giant Jetliner A380

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1 The Giant Jetliner A380 CHOONG-SIK SUH Case Study Meeting Sejong Univ, May 11th, 2005

2 Contents General Introduction Configuration Analysis Questions

3 Motivation For The Development Large transports account for Civil air transport will keep increasing at 5% per annum until % 13% Airbus Predictions Boeing Predictions

4 Motivation For The Development Airbus Commercial Plan Boeing Commercial Plan Focus on hub-to-hub connections Focus on point-to-point connections Syracuse Nantes Syracuse Nantes cincinnati JFK PARIS Lyon JFK PARIS Charlotte Marseilles cincinnati Lyon Charlotte Marseilles

5 Timeline of A380 A3XX Launch Production Maiden Flight Airline Service Development Costs $12 billions A380 Costs $280 millions B Costs $210 millions

6 Maiden Flight Date : April 27 th, 2005 Location : Toulouse,France

7 Why is she called A380? A350 A380? HOW COME?.

8 Performance & Dimensions & Weight & Other Data A380 B744 Remark Crusing Speed Same Range (km) 14,800 13, % Empty Weight(kg) 277, , % MTOW (kg) 560, , % Capacity (3 class) % Length (m) m Wing Span (m) m Height (m) m

9 Nose Fuselage Dimensions A380 A340 A320

10 Economic Size B pax 70% 123pax Break-even point A380 passengers Break-even point 323 pax 58% 232 pax 109 Additional profit potential Operating costs of the A380 are 17% lower per seat than those of the (15~20% lower seat-mile costs than other aircrafts)

11 Powerplant Systems Rolls-Royce Trent 900 Four 84,000lb Turbofan B744 Rolls-Royce RB ,000lb High by-pass ratio SFC ~ 0.51 lbm/hr*lbf (B744 ~ 0.33, B777 ~0.56) General Electric -Pratt & Whitney GP-7200 Four 81,500lb B744 P&W ,750lb GE CF6-80-C2B1Fs 61,500lb

12 Fuselage(Semi-Monocoque) MONO + COQUE 1 Truss + Monocoque Streamline Shape Pressure Dispersion

13 Aft Center of Gravity Relatively afterward C.G It allows to reduce area of horizontal stabilizer by 10% Weight Reduction

14 Wing Configuration Wing Area=5825ft ft2, 56% Increase AR = , 2.2% Decrease Span=261.65ft 211.8ft, 23% Increase LE Sweep =54 deg 47deg, more swept Taper Ratio= W/S = lb/ft lb/ft2, 9.6% Decrease

15 Supercritical Airfoil Conventional Airfoil Supercritical Airfoil Seperated b.l Smaller seperated b.l Relatively flat top, negative camber of forward 60% Cusplike shape to get extream positive camber To delay and reduce the transonic drag rise To make shock wave weaker

16 80m Gate Box Limit FAA Airplane Design Group for Geometric Design of Airport Airplane Design Group Wingspan (ft) Up to ft = 80m Runway width (ft)

17 The Drag Penalty Caused by 80m 80m Box Limit A380 should have had an AR of roughly 9.2 A380 AR is instead 7.53 The penalty in Induced Drag can be computed from Then So that

18 Effect of 80m Gate Box 25 AR b=102.1m L/D L/DMAX = 21.5 AR 7.53 b=79.8m L/DMAX = Altitude 1000ft Increase in AR allows boost of L/D by 16.8%

19 Wingtip Fence A B Raked Winglet Blended Winglet

20 Stall Speed and CLmax A380 B777 B747 Stall Speed (km/h) CLmax Low Wing Loading (w/s) Lower Stall Speed A380 W/S = lb/ft^2 B744 W/S = lb/ft^2 Single Slotted Flap

21 Flaps & Slats Simple Single Slotted Flap Due to aerodynamic noise One segmented For B , Triple Slotted Fowler Flap

22 Control Surfaces Conventional devices High-lift devices ~ 15 % of wing area Elavator ~ 27% of Sht Rudder ~ 17.2% of Svt Fly-by-wire More spoilers to dump lift

23 Wing Sweep Decreasing CDMAX LE Sweep Sweep c/4 Increasing stall angle of attack Decreasing critical Mach number Allowing wing tip stall A380 c/4 ~ 33.5 deg B744 c/4 ~ 37.5 deg

24 Taper Ratio Taper ratio of A380 ~ 0.26 Taper ratio of B744 ~ 0.24 Taper Ratio = Ct / Cr Induced drag fator 0.16 AR Taper ratio Lower wing weight Increased fuel volume Bigger space of landing gear. keep the taper ratio as small as possible

25 Wing Root Fillet Fairing A streamlined cover which connects wing with fusulage To pass the air flow smoothly To solve the buffeting problem To reduce interference drag Incurred additional weight

26 Conclusions A large size aircraft 80m gate box limit incuring more induced drag Advanced technology advanced materials Transfering many passensers at a time lower operating costs Good-bye B747

27 References p297~302 Flight International, 2-8 Jan. 2001, Number 4761, Volume 159 Aviation Week and Space Technology, Jan 1, 2001, Volume 154, Number 1 Kingsley-Jones. Market timing. Flight International, 2-8 January p. 62. Airbus tries new marketing approach with A380 designations. Flight International, 2-8 January p. 15. Cordle, Ina Paiva. Experts Defend Boeing, Question Viability of Airbus 800-Passenger Jumbo Jet. Knight-Ridder Business News, February 22, Via

28 Thanks and Any questions? Ask everything about A380 to Mr.suh

29 Expected Questions I got you ~ lol

30 Wake Vortex VORTEX ROLLING-UP UPWASH loss of loss altitude of altitude / rate / rate of climb of uncontrollable imb rolling moment DOWNWASH uncontrollable rolling mo ment

31 A380 Wake Vortex 0.10 induced rolling moment (-) B747 approach speed 165 kts A span of follower aircraft (m) For small followers (< 25m span), the vortex of an A380 may be less dangerous than that of a B747

32 Airport Compatibility ICAO level F, FAA Airport congestion Airport facilities supplement Taxi-way, Run-way width Run-way pavement

33 Correlation with Korea K.A.I is producing the A380 wing bottom panel Service from the end of 2007

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