External Aerodynamics Simulations in a Rotating Frame of Reference

Table 4

Experimental and computational results for the thrust coefficient.

Advance ratio 𝐽	Experimental 𝐶𝑇	Computational 𝐶𝑇
1.43	0.2192	0.217
1.5	0.2175	0.215
1.8	0.1782	0.174
2.0	0.1374	0.1376
2.4	0.0487	0.05