def page_viewer(point):
flow_stations = [
'fc.Fl_O', 'inlet.Fl_O', 'inlet_duct.Fl_O', 'fan.Fl_O',
'bypass_duct.Fl_O', 'splitter.Fl_O2', 'splitter.Fl_O1',
'splitter_core_duct.Fl_O', 'lpc.Fl_O', 'lpc_duct.Fl_O', 'hpc.Fl_O',
'bld3.Fl_O', 'burner.Fl_O', 'hpt.Fl_O', 'hpt_duct.Fl_O',
'lpt_duct.Fl_O', 'mixer.Fl_O', 'mixer_duct.Fl_O', 'afterburner.Fl_O',
'mixed_nozz.Fl_O'
]
compressors = ['fan', 'hpc', 'lpc']
burners = ['burner', 'afterburner']
turbines = ['hpt', 'lpt']
shafts = ['hp_shaft', 'lp_shaft']
print('*' * 80)
print('* ' + ' ' * 10 + point)
print('*' * 80)
print_perf(prob, point)
pyc.print_flow_station(prob, [point + "." + fl for fl in flow_stations])
pyc.print_compressor(prob, [point + "." + c for c in compressors])
# print_splitter(prob,[point+ ".splitter" ])
pyc.print_burner(prob, [point + "." + b for b in burners])
pyc.print_turbine(prob, [point + "." + turb for turb in turbines])
pyc.print_mixer(prob, [point + '.mixer'])
pyc.print_nozzle(prob, [point + '.mixed_nozz'])
pyc.print_shaft(prob, [point + "." + s for s in shafts])
pyc.print_bleed(prob, [point + '.hpc', point + '.bld3'])
def viewer(prob, pt, file=sys.stdout):
"""
print a report of all the relevant cycle properties
"""
summary_data = (prob[pt + '.fc.Fl_O:stat:MN'], prob[pt + '.fc.alt'],
prob[pt + '.inlet.Fl_O:stat:W'], prob[pt + '.perf.Fn'],
prob[pt + '.perf.Fg'], prob[pt + '.inlet.F_ram'],
prob[pt + '.perf.OPR'], prob[pt + '.perf.PSFC'])
print(file=file, flush=True)
print(file=file, flush=True)
print(file=file, flush=True)
print(
"----------------------------------------------------------------------------",
file=file,
flush=True)
print(" POINT:", pt, file=file, flush=True)
print(
"----------------------------------------------------------------------------",
file=file,
flush=True)
print(" PERFORMANCE CHARACTERISTICS",
file=file,
flush=True)
print(
" Mach Alt W Fn Fg Fram OPR PSFC ")
print(" %7.5f %7.1f %7.3f %7.1f %7.1f %7.1f %7.3f %7.5f" % summary_data)
fs_names = [
'fc.Fl_O', 'inlet.Fl_O', 'duct1.Fl_O', 'lpc.Fl_O', 'icduct.Fl_O',
'hpc_axi.Fl_O', 'bld25.Fl_O', 'hpc_centri.Fl_O', 'bld3.Fl_O',
'duct6.Fl_O', 'burner.Fl_O', 'hpt.Fl_O', 'duct43.Fl_O', 'lpt.Fl_O',
'itduct.Fl_O', 'pt.Fl_O', 'duct12.Fl_O', 'nozzle.Fl_O'
]
fs_full_names = [f'{pt}.{fs}' for fs in fs_names]
pyc.print_flow_station(prob, fs_full_names, file=file)
comp_names = ['lpc', 'hpc_axi', 'hpc_centri']
comp_full_names = [f'{pt}.{c}' for c in comp_names]
pyc.print_compressor(prob, comp_full_names, file=file)
pyc.print_burner(prob, [f'{pt}.burner'])
turb_names = ['hpt', 'lpt', 'pt']
turb_full_names = [f'{pt}.{t}' for t in turb_names]
pyc.print_turbine(prob, turb_full_names, file=file)
noz_names = ['nozzle']
noz_full_names = [f'{pt}.{n}' for n in noz_names]
pyc.print_nozzle(prob, noz_full_names, file=file)
shaft_names = ['hp_shaft', 'ip_shaft', 'lp_shaft']
shaft_full_names = [f'{pt}.{s}' for s in shaft_names]
pyc.print_shaft(prob, shaft_full_names, file=file)
bleed_names = ['bld25', 'bld3']
bleed_full_names = [f'{pt}.{b}' for b in bleed_names]
pyc.print_bleed(prob, bleed_full_names, file=file)
def viewer(prob, pt, file=sys.stdout):
"""
print a report of all the relevant cycle properties
"""
summary_data = (prob[pt + '.fc.Fl_O:stat:MN'], prob[pt + '.fc.alt'],
prob[pt + '.inlet.Fl_O:stat:W'], prob[pt + '.perf.Fn'],
prob[pt + '.perf.Fg'], prob[pt + '.inlet.F_ram'],
prob[pt + '.perf.OPR'], prob[pt + '.perf.TSFC'])
print(file=file, flush=True)
print(file=file, flush=True)
print(file=file, flush=True)
print(
"----------------------------------------------------------------------------",
file=file,
flush=True)
print(" POINT:", pt, file=file, flush=True)
print(
"----------------------------------------------------------------------------",
file=file,
flush=True)
print(" PERFORMANCE CHARACTERISTICS",
file=file,
flush=True)
print(
" Mach Alt W Fn Fg Fram OPR TSFC ",
file=file,
flush=True)
print(" %7.5f %7.1f %7.3f %7.1f %7.1f %7.1f %7.3f %7.5f" % summary_data,
file=file,
flush=True)
fs_names = [
'fc.Fl_O', 'inlet.Fl_O', 'comp.Fl_O', 'burner.Fl_O', 'turb.Fl_O',
'nozz.Fl_O'
]
fs_full_names = [f'{pt}.{fs}' for fs in fs_names]
pyc.print_flow_station(prob, fs_full_names, file=file)
comp_names = ['comp']
comp_full_names = [f'{pt}.{c}' for c in comp_names]
pyc.print_compressor(prob, comp_full_names, file=file)
pyc.print_burner(prob, [f'{pt}.burner'])
turb_names = ['turb']
turb_full_names = [f'{pt}.{t}' for t in turb_names]
pyc.print_turbine(prob, turb_full_names, file=file)
noz_names = ['nozz']
noz_full_names = [f'{pt}.{n}' for n in noz_names]
pyc.print_nozzle(prob, noz_full_names, file=file)
shaft_names = ['shaft']
shaft_full_names = [f'{pt}.{s}' for s in shaft_names]
pyc.print_shaft(prob, shaft_full_names, file=file)
def viewer(prob, pt):
fs_names = ['fc.Fl_O', 'inlet.Fl_O', 'fan.Fl_O', 'nozz.Fl_O']
fs_full_names = [f'{pt}.{fs}' for fs in fs_names]
pyc.print_flow_station(prob, fs_full_names)
pyc.print_compressor(prob, [f'{pt}.fan'])
pyc.print_nozzle(prob, [f'{pt}.nozz'])
def viewer(prob, pt):
"""
print a report of all the relevant cycle properties
"""
fs_names = ['fc.Fl_O', 'inlet.Fl_O', 'fan.Fl_O', 'nozz.Fl_O']
fs_full_names = [f'{pt}.{fs}' for fs in fs_names]
pyc.print_flow_station(prob, fs_full_names)
pyc.print_compressor(prob, [f'{pt}.fan'])
pyc.print_nozzle(prob, [f'{pt}.nozz'])
def viewer(prob, pt, file=sys.stdout):
"""
print a report of all the relevant cycle properties
"""
summary_data = (prob[pt + '.fc.Fl_O:stat:MN'], prob[pt + '.fc.alt'],
prob[pt + '.inlet.Fl_O:stat:W'], prob[pt + '.perf.Fn'],
prob[pt + '.perf.Fg'], prob[pt + '.inlet.F_ram'],
prob[pt + '.perf.OPR'], prob[pt + '.perf.TSFC'],
prob[pt + '.splitter.BPR'])
print(file=file, flush=True)
print(file=file, flush=True)
print(file=file, flush=True)
print(
"----------------------------------------------------------------------------",
file=file,
flush=True)
print(" POINT:", pt, file=file, flush=True)
print(
"----------------------------------------------------------------------------",
file=file,
flush=True)
print(" PERFORMANCE CHARACTERISTICS",
file=file,
flush=True)
print(
" Mach Alt W Fn Fg Fram OPR TSFC BPR ",
file=file,
flush=True)
print(" %7.5f %7.1f %7.3f %7.1f %7.1f %7.1f %7.3f %7.5f %7.3f" %
summary_data,
file=file,
flush=True)
fs_names = [
'fc.Fl_O', 'inlet.Fl_O', 'fan.Fl_O', 'splitter.Fl_O1', 'duct2.Fl_O',
'lpc.Fl_O', 'bld25.Fl_O', 'duct25.Fl_O', 'hpc.Fl_O', 'bld3.Fl_O',
'burner.Fl_O', 'hpt.Fl_O', 'duct45.Fl_O', 'lpt.Fl_O', 'duct5.Fl_O',
'core_nozz.Fl_O', 'splitter.Fl_O2', 'byp_bld.Fl_O', 'duct17.Fl_O',
'byp_nozz.Fl_O'
]
fs_full_names = [f'{pt}.{fs}' for fs in fs_names]
pyc.print_flow_station(prob, fs_full_names, file=file)
comp_names = ['fan', 'lpc', 'hpc']
comp_full_names = [f'{pt}.{c}' for c in comp_names]
pyc.print_compressor(prob, comp_full_names, file=file)
pyc.print_burner(prob, [f'{pt}.burner'])
turb_names = ['hpt', 'lpt']
turb_full_names = [f'{pt}.{t}' for t in turb_names]
pyc.print_turbine(prob, turb_full_names, file=file)
noz_names = ['core_nozz', 'byp_nozz']
noz_full_names = [f'{pt}.{n}' for n in noz_names]
pyc.print_nozzle(prob, noz_full_names, file=file)
shaft_names = ['hp_shaft', 'lp_shaft', 'fan_shaft']
shaft_full_names = [f'{pt}.{s}' for s in shaft_names]
pyc.print_shaft(prob, shaft_full_names, file=file)
bleed_names = ['hpc', 'bld3', 'bld3', 'bld25']
bleed_full_names = [f'{pt}.{b}' for b in bleed_names]
pyc.print_bleed(prob, bleed_full_names, file=file)
