**Compressor1_CL**

Procedure Compressor1_CL is a model of a single-stage radial compressor operating outside of the vapor dome. Pressure rise is determined from a generic head (Y) versus flow coefficient (*f*) curve that can be shifted vertically and horizontally. Efficiency is determined from efficiency (*h*) versus flow coefficient curve that can be shifted vertically and horizontally relative to a generic curve. The generic curve is based on the radial compressor discussed in Dyreby (2014) and is valid from 0.00544 < *f* < 0.0512, although surge is likely for *f *<0.018. The generic curve provides a maximum efficiency at *f* = 0.0299 and a maximum head coefficient at *f* = 0.02261. The curve can be shifted horizontally using the phi_scale parameter

**References:**

Dyreby, J., "Modeling the Supercritical Carbon Dioxide Brayton Cycle with Recompression," Ph.D. Thesis, University of Wisconsin, Mechanical Engineering Department, (2014).

**Inputs:**

T_in: inlet temperature (K, C, F, or R)

P_in: inlet pressure (bar, atm, Pa, kPa, MPa)

m_dot: mass flow rate (kg/s or lb_m/hr)

F$: fluid string identifier

N: rotational speed (rev/s)

D: diameter (ft or m)

eta_max: maximum isentropic efficiency, typical curve is shifted up to achieve this

psi_max: maximum head coefficient, typical curve is shifted up to achieve this

phi_scale: scales the eta vs phi and psi vs phi curves horizontally

a value of 1 applies no scaling - peak of efficiency occurs at phi = 0.0299 and peak of psi curve occurs at phi = 0.02261

a value of 1.1 stretches the curve out by 10%

**Outputs**

P_out: outlet pressure (bar, atm, Pa, kPa, MPa)

T_out: outlet temperature (K, C, F, or R)

W_dot: power (W, kW or Btu/hr)

phi: flow coefficient

eta: isentropic efficiency

psi: head coefficient

Ma: Mach number, evaluated at outlet sound speed

**Example: **

$Load Component Library

$UnitSystem SI Mass J K Pa

$VarInfo P_out units=Pa

$VarInfo T_out units=K

$VarInfo W_dot units=W

T_in=300 [K]

P_in=100000 [Pa]

m_dot=0.1 [kg/s]

F$='Air'

N=1000 [rev/s]

D=0.1 [m]

eta_max=0.9

psi_max=0.7

phi_scale=1

*Call***compressor1_cl**(T_in, P_in, m_dot, F$, N, D, eta_max, psi_max, phi_scale: P_out, T_out, W_dot, phi, eta, psi, Ma)

{**Solution:**

eta=0.8806

Ma=0.8176

phi=0.0349

psi=0.6121

P_out=189623 [Pa]

T_out=368.1 [K]

W_dot=6861 [W]}