Added bleed channel test

tests/test_compressor_bleed.py

@@ -0,0 +1,67 @@
+# SPDX-FileCopyrightText: © 2024 Antonio López Rivera <[email protected]>
+# SPDX-License-Identifier: GPL-3.0-only
+
+import sys
+from pathlib import Path
+sys.path.append(str(Path(__file__).parents[1]))
+
+"""
+Turbojet engine test
+--------------------
+Twin-spool, reheated turbojet engine with an electrical power plant.
+"""
+
+from huracan.engine import shaft
+from huracan.thermo.fluids import gas, fuel
+from huracan.components import inlet, compressor, combustion_chamber, turbine, afterburner, nozzle, electrical_system, bleed_duct
+
+mf = 160
+M  = 0
+t  = 288
+p  = 101325
+
+fuel_cc = fuel(LHV=43e6)
+
+g = gas(mf=mf,
+        cp=lambda T: 1150 if T > 600 else 1000,
+        k=lambda T: 1.33 if T > 600 else 1.4,
+        m=M, t_0=t, p_0=p)
+
+"""
+Define engine components
+"""
+i  = inlet             (PI=0.92)
+c1 = compressor        (eta=0.85, PI=4); c1_bleed = 0.5 / 100
+c2 = compressor        (eta=0.85, PI=4)
+bd = bleed_duct        (t01=288.15, eta=0.95)
+cc = combustion_chamber(fuel=fuel_cc, eta=0.97, t01=1450)
+t1 = turbine           (eta=0.9)
+t2 = turbine           (eta=0.9)
+n  = nozzle            (eta=0.95)
+elctr  = electrical_system(w=970000, eta_g=0.7, eta_c=0.98)
+
+shaft1 = shaft(c1, t2,        eta=0.99)
+shaft2 = shaft(c2, t1, elctr, eta=0.99)
+
+"""
+Define stream structure
+"""
+stream = g-i-c1
+
+core_stream, compressor_bleed_stream = stream*c1_bleed
+
+compressor_bleed_stream-bd
+
+core_stream-c2-cc-t1-t2-n
+
+# stream-c2-cc-t1-t2-n
+
+"""
+Simulate engine
+"""
+stream.run()
+
+stream.plot(x='S', y='t0', show=True, colorblind=True)
+stream.plot(x='V', y='p0', show=True, colorblind=True)
+stream.plot(x='p0', y='H', show=True, colorblind=True)
+stream.plot(x='p0', y='t0', show=True, colorblind=True)