External Aerodynamics Simulations in a Rotating Frame of Reference

Table 5

Experimental and computational results for the thrust coefficient.

Advance ratio 𝐽	Experimental 𝐶𝑇	Computational 𝐶𝑇
1.43	0.206	0.2
1.5	0.2052	0.196
1.8	0.175	0.18
2.0	0.14	0.135
2.4	0.049	0.054