Typical aspect ratios can be found in the following table:
Estimated geometric and aerodynamic characteristics of representative aircraft LOFTIN 1980
A | l / d | 3.14d² / 4S | At / SW | L' | cD,0 | cL,m | (L / D)max |
---|---|---|---|---|---|---|---|
Narrow-body transport | |||||||
7.4 | 11.8 | 0.039 | 5.00 | 1.0 | 0.0131 | 0.51 | 19.4 |
7.5 | 13.59 | 0.051 | 5.95 | 1.0 | 0.0156 | 0.56 | 17.92 |
7.0 | 9.4 | 0.072 | 5.80 | 0.74 | 0.0160 | 0.55 | 17.10 |
7.0 | 11.1 | 0.072 | 6.29 | 0.74 | 0.0173 | 0.57 | 16.42 |
8.8 | 7.9 | 0.121 | 6.72 | 0.64 | 0.0190 | 0.67 | 17.59 |
8.7 | 9 | 0.111 | 6.93 | 0.64 | 0.0196 | 0.67 | 17.23 |
8.5 | 7.5 | 0.096 | 5.88 | 0.64 | 0.0166 | 0.61 | 18.49 |
Wide-body transport | |||||||
7.0 | 10.3 | 0.069 | 5.95 | 1.34 | 0.0148 | 0.53 | 17.74 |
7.6 | 8.7 | 0.095 | 6.31 | 1.13 | 0.0162 | 0.57 | 17.70 |
7.0 | 9.1 | 0.088 | 6.23 | 1.07 | 0.0161 | 0.55 | 17.02 |
7.7 | 9.2 | 0.096 | 6.53 | 1.0 | 0.0171 | 0.59 | 17.33 |
Business jet | |||||||
5.0 | 8.7 | 0.085 | 6.00 | 0.24 | 0.0199 | 0.52 | 12.94 |
6.0 | 9.4 | 0.072 | 5.80 | 0.47 | 0.0172 | 0.52 | 15.25 |
Wing span and aspect ratio of selected aircraft Jane's 1995-98
Aircraft
Airbus
A 300-600BAirbus
A 310-300Airbus
A 320-200Airbus
A 340-300Antonov
AN 124BAe (Avro)
RJ85Boeing
B 737-600Boeing
B 747-400Boeing
B 777Cessna 525
CitationJetLearjet
60McDonnell
Douglas MD11Tupolev
TU 204
Wing span [ m ]
44.84 43.89 33.91 60.30 73.30 26.21 34.31 64.44 60.93 14.25 13.34 51.66 42.0
Aspect ratio [ - ]
7.7 8.8 9.4 10.0 8.6 9.0 9.4 7.7 8.7 9.1 7.2 7.9 9.7
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