Statistic of aspect ratio

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
7.411.80.0395.001.00.01310.5119.4
7.513.590.0515.951.00.01560.5617.92
7.09.40.0725.800.740.01600.5517.10
7.011.10.0726.290.740.01730.5716.42
8.87.90.1216.720.640.01900.6717.59
8.790.1116.930.640.01960.6717.23
8.57.50.0965.880.640.01660.6118.49
Wide-body transport
7.010.30.0695.951.340.01480.5317.74
7.68.70.0956.311.130.01620.5717.70
7.09.10.0886.231.070.01610.5517.02
7.79.20.0966.531.00.01710.5917.33
Business jet
5.08.70.0856.000.240.01990.5212.94
6.09.40.0725.800.470.01720.5215.25

Wing span and aspect ratio of selected aircraft Jane's 1995-98
Aircraft Airbus
A 300-600B
Airbus
A 310-300
Airbus
A 320-200
Airbus
A 340-300
Antonov
AN 124
BAe (Avro)
RJ85
Boeing
B 737-600
Boeing
B 747-400
Boeing
B 777
Cessna 525
CitationJet
Learjet
60
McDonnell
Douglas MD11
Tupolev
TU 204
Wing span [ m ] 44.8443.8933.9160.3073.3026.2134.3164.4460.9314.2513.3451.6642.0
Aspect ratio [ - ] 7.78.89.410.08.69.09.47.78.79.17.27.99.7

 
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