Page 182 - Aeronautical Engineer Data Book

Tupolev Tu-204 -200 28 S2 0.77 slats 34.2 7.7 1.73 0.34 36 21.8 0.188 0.101

McDon. /Doug. MD-11 9.35 35 S2 0.7 slats 56.2 11.16 2.22 0.369 40 20.92 0.166 0.067

McDon. /Doug. MD-90-30 11 24.5 S2 0.63 slats 21.4 4.7 1.03 0.77 43 15.6 0.191 0.09

Ilyushin II-96M 30 S2 0.79 slats 56.2 8 1.14 0.4 45 25.9 0.144 0.067

Fokker F100 10.28 17.45 F2 0.58 17.08 none 12.3 3.3 0.89 0.74 41 13.6 0.132 0.064

Fokker F70 10.28 17.45 F2 0.58 17.08 none 12.3 3.3 0.89 0.74 41 11.4 0.132 0.053

Embraer EMB-145 11 22.73 S2 0.72 8.36 none 7.2 3.1 1.33 0.6 32 11.5 0.141 0.081

Cadair Reg. Jet 100ER 10.83 24.75 S2 0.66 10.6 slats 9.18 2.6 0.74 0.73 41 10.7 0.168 0.088

Boeing 737– 800 25 S2 0.599 slats/flaps 23.13 6 1.56 0.31 35 17.7 0.186 0.096

Boeing 717– 200 11.6 24.5 S2 0.65 slats 19.5 4.35 0.97 0.78 45 12.8 0.21 0.095

Airbus A340– 500 31.1 S2 0.625 slats 47.65 9.44 1.87 0.35 45 27.5 0.109 0.049

Airbus A340– 300 29.7 S2 0.665 slats 45.2 8.45 1.58 0.35 45 27.5 0.124 0.059

Airbus A330– 200 29.7 S2 0.665 slats 47.65 9.44 1.87 0.35 45 25.2 0.131 0.057

Airbus A321– 200 25 F2 0.78 21.1 slats 12.64 21.5 6.26 1.82 0.303 34 15.2 0.176 0.079

Airbus A320– 200 25 F1 0.78 21.1 slats 12.64 t21.5 6.26 1.82 0.303 34 12.53 0.176 0.065
Table 10.1 Continued Manufacturer Type Model Average t/c % 1/4 chord sweep (°) High lift devices: Trailing edge flaps type Flap span/Wing span Area (m 2 ) Leading edge flaps Ty