An Open Access Journal
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