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Table 2 Aerodynamic parameters

From: A new aircraft architecture based on the ACHEON Coanda effect nozzle: flight model and energy evaluation

CD0

0.027

E

7.7

K

0.00617

CL0

0.167

CDmax

0.0338

CLmax

1.104

CLmax,carriage

0.0415

CLmax carriage

2.35

W TOmax / S

185.86

T SL / W TOmax

1.67