Design Optimization of a Transonic-Fan Rotor Using Numerical Computations of the Full Compressible Navier-Stokes Equations and Simplex Algorithm

Table 2

Baseline data of the selected case.

Requirements		Inlet conditions		Selected parameters
Mass flow rate	120 kg/sec	Total inlet temperature	300 K	𝑁 (r.p.m)	<10500
Fan pressure ratio	2.6	Total inlet pressure	101.325 kPa	Hub-to-tip ratio	0.2–0.7
				Diffusion factor	<0.55
				Inlet axial Mach number	0.7