Table 1.

Model parameters used for validation [25].

Variable	Symbol	Unit	Value
Airfoil type	–	–	NACA0015
Blade chord length	c	m	0.2
Density	ρ	kg/m3	1.225
Freestream velocity	$V_{\infty }$	m/s	1.95-19.5
Initial angle of attack	β	degree	0
Number of blades	N	–	2
Pressure	P	Pa	101325
Rotor radius	R	m	3
Tip speed ratio	TSR or λ	–	1–10
Turbine speed	$\omega$	rpm	125
Vertical height	h	m	6