Table 3.

FR and force coefficient values

Flight angle (degrees)
–60–3003060
FR (N)4.45±0.254.41±0.334.18±0.295.20±0.205.13±0.41
C L 1.18±0.161.72±0.101.44±0.290.77±0.130.74±0.20
C D 1.15±0.211.07±0.411.01±0.080.44±0.190.67±0.06
C v 2.65±0.262.51±0.192.50±0.251.51±0.352.09±0.30
C h 1.46±0.320.50±0.100.97±0.250.81±0.221.74±0.25