Description |
|
Flat windows with protruding frame |
0.016 |
Flat windows flush with surface |
0.011 |
Single curvature window, flush with surface rounded corners |
0.002 |
Single curvature window, flush with surface sharp corners |
0.005 |
Double curvature window, flush with surface |
0.002 |
Drag coefficient of the windshield referenced to the frontal area of the fuselage