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
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
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
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
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
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
# 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 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)
# # 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 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.) 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)
# 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 MDOTools.ValidGrad.FDValidGrad import FDValidGrad from DLLM.DLLMGeom.wing_param import Wing_param from DLLM.DLLMKernel.DLLMTargetCl import DLLMTargetCl from MDOTools.OC.operating_condition import OperatingCondition import numpy import sys 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)
# 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. # # https://github.com/matthieu-meaux/DLLM.git # # @author : Matthieu MEAUX # # Imports from MDOTools.OC.operating_condition import OperatingCondition from DLLM.DLLMGeom.wing_broken import Wing_Broken from DLLM.DLLMKernel.DLLMTargetCl import DLLMTargetCl OC=OperatingCondition('cond1', atmospheric_model='ISA') OC.set_Mach(0.8) OC.set_AoA(3.0) 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() wing_param.plot() DLLM = DLLMTargetCl('TCl',wing_param,OC) DLLM.set_target_Cl(0.5)
# 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 MDOTools.ValidGrad.FDValidGrad import FDValidGrad from DLLM.DLLMGeom.wing_param import Wing_param from DLLM.DLLMKernel.DLLMTargetCl import DLLMTargetCl from MDOTools.OC.operating_condition import OperatingCondition 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',3.) wing_param.set_value('sweep',30.) 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)
# GNU General Public License for more details. # # 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 # # Imports from DLLM.DLLMGeom.wing_param import Wing_param from DLLM.DLLMKernel.DLLMSolver import DLLMSolver from MDOTools.OC.operating_condition import OperatingCondition OC = OperatingCondition('cond1') OC.set_Mach(0.3) OC.set_AoA(4.) OC.set_altitude(1000.) 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', 2.392) #34.1 wing_param.set_value('sweep', 26.7) wing_param.set_value('break_percent', 33.) #33. wing_param.set_value('root_chord', 0.806) #6.1 wing_param.set_value('break_chord', 0.689) wing_param.set_value('tip_chord', 0.451) #1.5 wing_param.set_value('root_height', 0.0782)
# GNU General Public License for more details. # # 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 # # Imports from DLLM.DLLMGeom.wing_param import Wing_param from DLLM.DLLMKernel.DLLMSolver import DLLMSolver from MDOTools.OC.operating_condition import OperatingCondition OC=OperatingCondition('cond1') OC.set_Mach(0.3) OC.set_AoA(4.) OC.set_altitude(1000.) 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',2.392) #34.1 wing_param.set_value('sweep',26.7) wing_param.set_value('break_percent',33.) #33. wing_param.set_value('root_chord',0.806) #6.1 wing_param.set_value('break_chord',0.689) wing_param.set_value('tip_chord',0.451) #1.5 wing_param.set_value('root_height',0.0782)
# # 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 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
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the # GNU General Public License for more details. # # 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 MDOTools.ValidGrad.FDValidGrad import FDValidGrad from DLLM.DLLMGeom.wing_param import Wing_param from MDOTools.OC.operating_condition import OperatingCondition 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)
# # 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 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