Table 1: BWB aircraft in mid-cruise conditions (z = 35 k ft, m = 715 t, Ma = 0.85).
|
Aerodynamic Coefficient |
Symbol |
AOA |
At cruise |
|
|
a = 0° |
a = 3° |
a0 = 0.71789° |
||
|
Lift |
CL |
0.04411 |
0.30224 |
0.10588 |
|
Drag |
CD |
0.00423 |
0.01033 |
0.00569 |
|
Pitching moment |
CM |
-0.00819 |
-0.07596 |
-0.02441 |