#!/usr/bin/env python
# -*- coding: utf-8 -*-
import sys
sys.path.insert(0,"src")
import turbofan
turbo=turbofan.turbofan("Hummingbird TJ70")
#Turbofan-Randbedingungen
turbo.thrust=120.0 #N
turbo.T_0=293.15 #K
turbo.T_t4=800.0 #K
turbo.R=287.1
turbo.kappa=1.4
turbo.c_0=0.0 #m/s
#Verdichterrandbedingungen
turbo.hpcomp.Pi=3.15
#Wirkungsgrade der Komponenten
turbo.hpcomp.eta_is=0.75
turbo.combc.deltap_t=0.01
turbo.hpturb.eta_is=0.75
#Thermodynamische Konstanten der Komponenten
turbo.hpcomp.kappa=1.4
turbo.hpcomp.R=287.1
turbo.combc.kappa=1.3
turbo.combc.R=287.1
turbo.hpturb.kappa=1.35
turbo.hpturb.R=287.1
#Aerodynamische Randbedingungen
turbo.Ma_max=0.8
turbo.p_0=101325.0
turbo.calcCycle()
turbo.printParams()
#turbo.calcAero()
#turbo.printT()
#turbo.printH()
#turbo.fan.printAero()
