Ejemplos de OperatingCondition.set_T0_deg en Python

Ejemplo n.º 1

 def __init_wing_param(self):
     OC=OperatingCondition('cond1')
     OC.set_Mach(0.8)
     OC.set_AoA(3.5)
     OC.set_altitude(10000.)
     OC.set_T0_deg(15.)
     OC.set_P0(101325.)
     OC.set_humidity(0.)
     OC.compute_atmosphere()
     
     wing_param=Wing_param('test_param',geom_type='Broken',n_sect=20)
     wing_param.build_wing()
     wing_param.set_value('span',34.1)
     wing_param.set_value('sweep',34.)
     wing_param.set_value('break_percent',33.)
     wing_param.set_value('root_chord',6.1)
     wing_param.set_value('break_chord',4.6)
     wing_param.set_value('tip_chord',1.5)
     wing_param.set_value('root_height',1.28)
     wing_param.set_value('break_height',0.97)
     wing_param.set_value('tip_height',0.33)
     wing_param.convert_to_design_variable('span',(10.,50.))
     wing_param.convert_to_design_variable('sweep',(0.,40.))
     wing_param.convert_to_design_variable('break_percent',(20.,40.))
     wing_param.convert_to_design_variable('root_chord',(5.,7.))
     wing_param.convert_to_design_variable('break_chord',(3.,5.))
     wing_param.convert_to_design_variable('tip_chord',(1.,2.))
     wing_param.convert_to_design_variable('root_height',(1.,1.5))
     wing_param.convert_to_design_variable('break_height',(0.8,1.2))
     wing_param.convert_to_design_variable('tip_height',(0.2,0.5))
     wing_param.build_linear_airfoil(OC, AoA0=-2., Cm0=-0.1, set_as_ref=True)
     wing_param.build_airfoils_from_ref()
     wing_param.update()
     
     return OC,wing_param

Ejemplo n.º 2

Archivo: test_wing_param.py Proyecto: FrancoisGallard/DLLM

 def __init_wing_param(self):
     OC=OperatingCondition('cond1')
     OC.set_Mach(0.7)
     OC.set_AoA(3.0)
     OC.set_altitude(5000.)
     OC.set_T0_deg(20.)
     OC.set_P0(101325.)
     OC.set_humidity(0.)
     OC.compute_atmosphere()
     
     wing_param=Wing_param('test_param',geom_type='Broken',n_sect=20)
     wing_param.build_wing()
     wing_param.set_value('span',34.1)
     wing_param.set_value('sweep',32.)
     wing_param.set_value('break_percent',33.)
     wing_param.set_value('root_chord',6.1)
     wing_param.set_value('break_chord',4.6)
     wing_param.set_value('tip_chord',1.5)
     wing_param.set_value('root_height',1.28)
     wing_param.set_value('break_height',0.97)
     wing_param.set_value('tip_height',0.33)
     wing_param.convert_to_design_variable('span',(10.,50.))
     wing_param.convert_to_design_variable('sweep',(0.,40.))
     wing_param.convert_to_design_variable('break_percent',(20.,40.))
     wing_param.convert_to_design_variable('root_chord',(5.,7.))
     wing_param.convert_to_design_variable('break_chord',(3.,5.))
     wing_param.convert_to_design_variable('tip_chord',(1.,2.))
     wing_param.convert_to_design_variable('root_height',(1.,1.5))
     wing_param.convert_to_design_variable('break_height',(0.8,1.2))
     wing_param.convert_to_design_variable('tip_height',(0.2,0.5))
     wing_param.build_linear_airfoil(OC, AoA0=-2., Cm0=-0.1, set_as_ref=True)
     wing_param.build_airfoils_from_ref()
     wing_param.update()
     
     return wing_param

Ejemplo n.º 3

 def __init_OC(self):
     OC = OperatingCondition('cond1')
     OC.set_Mach(0.7)
     OC.set_AoA(3.0)
     OC.set_altitude(5000.)
     OC.set_T0_deg(20.)
     OC.set_P0(101325.)
     OC.set_humidity(0.)
     OC.compute_atmosphere()
     return OC

Ejemplo n.º 4

Archivo: test_wing_param.py Proyecto: FrancoisGallard/DLLM

 def __init_OC(self):
     OC=OperatingCondition('cond1')
     OC.set_Mach(0.7)
     OC.set_AoA(3.0)
     OC.set_altitude(5000.)
     OC.set_T0_deg(20.)
     OC.set_P0(101325.)
     OC.set_humidity(0.)
     OC.compute_atmosphere()
     return OC

Ejemplo n.º 5

Archivo: test_DLLM_simple_TCl_TLift.py Proyecto: matthieu-meaux/DLLM

 def __init_wing_param(self):
     OC=OperatingCondition('cond1')
     OC.set_Mach(0.8)
     OC.set_AoA(3.5)
     OC.set_altitude(10000.)
     OC.set_T0_deg(15.)
     OC.set_P0(101325.)
     OC.set_humidity(0.)
     OC.compute_atmosphere()
     
     wing_param=Wing_Broken('broken_wing',n_sect=20)
     wing_param.import_BC_from_file('input_parameters.par')
     wing_param.build_linear_airfoil(OC, AoA0=0.0, set_as_ref=True)
     wing_param.build_airfoils_from_ref()
     wing_param.update()
     
     return OC,wing_param

Ejemplo n.º 6

Archivo: test_DLLM_meta.py Proyecto: regislebrun/DLLM

    def __init_wing_param(self):
        OC = OperatingCondition('cond1')
        OC.set_Mach(0.8)
        OC.set_AoA(3.5)
        OC.set_altitude(10000.)
        OC.set_T0_deg(15.)
        OC.set_P0(101325.)
        OC.set_humidity(0.)
        OC.compute_atmosphere()

        wing_param = Wing_param('test_param', geom_type='Broken', n_sect=20)
        wing_param.build_wing()
        wing_param.set_value('span', 34.1)
        wing_param.set_value('sweep', 34.)
        wing_param.set_value('break_percent', 33.)
        wing_param.set_value('root_chord', 6.1)
        wing_param.set_value('break_chord', 4.6)
        wing_param.set_value('tip_chord', 1.5)
        wing_param.set_value('root_height', 1.28)
        wing_param.set_value('break_height', 0.97)
        wing_param.set_value('tip_height', 0.33)
        wing_param.convert_to_design_variable('span', (10., 50.))
        wing_param.convert_to_design_variable('sweep', (0., 40.))
        wing_param.convert_to_design_variable('break_percent', (20., 40.))
        wing_param.convert_to_design_variable('root_chord', (5., 7.))
        wing_param.convert_to_design_variable('break_chord', (3., 5.))
        wing_param.convert_to_design_variable('tip_chord', (1., 2.))
        wing_param.convert_to_design_variable('root_height', (1., 1.5))
        wing_param.convert_to_design_variable('break_height', (0.8, 1.2))
        wing_param.convert_to_design_variable('tip_height', (0.2, 0.5))
        wing_param.build_meta_airfoil(OC,
                                      '../examples/MetaModelFixed.xml',
                                      relative_thickness=.12,
                                      camber=0.,
                                      Sref=1.,
                                      Lref=1.,
                                      sweep=.0,
                                      set_as_ref=True)
        wing_param.build_airfoils_from_ref()
        wing_param.update()

        return OC, wing_param

Ejemplo n.º 7

Archivo: Rect_sweep0.py Proyecto: FrancoisGallard/DLLM

#  Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
# 
#  http://github.com/TBD
#
from DLLM.DLLMGeom.wing_param import Wing_param
from DLLM.DLLMKernel.DLLMTargetCl import DLLMTargetCl
from MDOTools.OC.operating_condition import OperatingCondition
from MDOTools.ValidGrad.FDValidGrad import FDValidGrad
import numpy
import sys

OC=OperatingCondition('cond1')
OC.set_Mach(0.3)
OC.set_AoA(0.)
OC.set_altitude(3000.)
OC.set_T0_deg(15.)
OC.set_P0(101325.)
OC.set_humidity(0.)
OC.compute_atmosphere()

wing_param=Wing_param('test_param',geom_type='Broken',n_sect=20)
wing_param.build_wing()
wing_param.set_value('span',40.)
wing_param.set_value('sweep',0.)
wing_param.set_value('break_percent',33.)
wing_param.set_value('root_chord',1.0)
wing_param.set_value('break_chord',1.0)
wing_param.set_value('tip_chord',1.0)
wing_param.set_value('root_height',0.15)
wing_param.set_value('break_height',0.15)
wing_param.set_value('tip_height',0.15)

Ejemplo n.º 8

Archivo: Induced_drag_theoretical.py Proyecto: regislebrun/DLLM

# 
#  You should have received a copy of the GNU General Public License
#  along with this program; if not, write to the Free Software
#  Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
# 
#  http://github.com/TBD
#
from DLLM.DLLMGeom.wing_param import Wing_param
from MDOTools.OC.operating_condition import OperatingCondition
import numpy
import string

OC=OperatingCondition('cond1')

OC.set_altitude(3000.)
OC.set_T0_deg(15.)
OC.set_P0(101325.)
OC.set_humidity(0.)

nsect=50

wing_param=Wing_param('test_param',geom_type='Elliptic',n_sect=nsect)
wing_param.set_distrib_type('cos_law')
wing_param.build_wing()
wing_param.set_value('span',40.)
wing_param.set_value('root_chord',4.)
wing_param.set_value('root_height',0.0)
wing_param.set_value('tip_height',0.0)
wing_param.build_linear_airfoil(OC, AoA0=0., Cm0=-0.1, set_as_ref=True)
wing_param.build_airfoils_from_ref()
wing_param.update()

Ejemplo n.º 9

Archivo: valid_dpR_dpiAoA.py Proyecto: FrancoisGallard/DLLM

#  along with this program; if not, write to the Free Software
#  Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
#
#  http://github.com/TBD
#
from MDOTools.ValidGrad.FDValidGrad import FDValidGrad
from DLLM.DLLMGeom.wing_param import Wing_param
from DLLM.DLLMKernel.DLLMSolver import DLLMSolver
from MDOTools.OC.operating_condition import OperatingCondition
import numpy

OC = OperatingCondition("cond1")
OC.set_Mach(0.8)
OC.set_AoA(3.5)
OC.set_altitude(10000.0)
OC.set_T0_deg(15.0)
OC.set_P0(101325.0)
OC.set_humidity(0.0)
OC.compute_atmosphere()

wing_param = Wing_param("test_param", geom_type="Broken", n_sect=20)
wing_param.build_wing()
wing_param.set_value("span", 34.1)
wing_param.set_value("sweep", 34.0)
wing_param.set_value("break_percent", 33.0)
wing_param.set_value("root_chord", 6.1)
wing_param.set_value("break_chord", 4.6)
wing_param.set_value("tip_chord", 1.5)
wing_param.set_value("root_height", 1.28)
wing_param.set_value("break_height", 0.97)
wing_param.set_value("tip_height", 0.33)

Ejemplo n.º 10

Archivo: valid_grad_DLLM_meta.py Proyecto: regislebrun/DLLM

#  along with this program; if not, write to the Free Software
#  Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
#
#  http://github.com/TBD
#
from DLLM.DLLMGeom.wing_param import Wing_param
from DLLM.DLLMKernel.DLLMSolver import DLLMSolver
from MDOTools.ValidGrad.FDValidGrad import FDValidGrad
from MDOTools.OC.operating_condition import OperatingCondition
import numpy

OC = OperatingCondition('cond1')
OC.set_Mach(0.6)  #.7
OC.set_AoA(6.0)  #3.
OC.set_altitude(10000.)  #5000
OC.set_T0_deg(20.)
OC.set_P0(101325.)
OC.set_humidity(0.)
OC.compute_atmosphere()

wing_param = Wing_param('test_param', geom_type='Broken', n_sect=20)
wing_param.build_wing()
wing_param.set_value('span', 34.1)
wing_param.set_value('sweep', 32.)  #32.
wing_param.set_value('break_percent', 33.)
wing_param.set_value('root_chord', 5.4)  #6.1
wing_param.set_value('break_chord', 4.6)  #4.6
wing_param.set_value('tip_chord', 1.2)  #1.5
wing_param.set_value('root_height', .98)  #1.28
wing_param.set_value('break_height', 0.7)  #0.97
wing_param.set_value('tip_height', 0.18)  #0.33

Ejemplo n.º 11

Archivo: valid_grad_DLLM_meta.py Proyecto: FrancoisGallard/DLLM

#  along with this program; if not, write to the Free Software
#  Foundation, Inc., 51 Franklin Street, Fifth Floor, Boston, MA  02110-1301, USA.
# 
#  http://github.com/TBD
#
from DLLM.DLLMGeom.wing_param import Wing_param
from DLLM.DLLMKernel.DLLMSolver import DLLMSolver
from MDOTools.ValidGrad.FDValidGrad import FDValidGrad
from MDOTools.OC.operating_condition import OperatingCondition
import numpy

OC=OperatingCondition('cond1')
OC.set_Mach(0.6) #.7
OC.set_AoA(6.0) #3.
OC.set_altitude(10000.) #5000
OC.set_T0_deg(20.)
OC.set_P0(101325.)
OC.set_humidity(0.)
OC.compute_atmosphere()

wing_param=Wing_param('test_param',geom_type='Broken',n_sect=20)
wing_param.build_wing()
wing_param.set_value('span',34.1)
wing_param.set_value('sweep',32.) #32.
wing_param.set_value('break_percent',33.)
wing_param.set_value('root_chord',5.4)#6.1
wing_param.set_value('break_chord',4.6)#4.6
wing_param.set_value('tip_chord',1.2)#1.5
wing_param.set_value('root_height',.98)#1.28
wing_param.set_value('break_height',0.7)#0.97
wing_param.set_value('tip_height',0.18)#0.33