Core conceptual optimization of rotorcraft environment in matlab

The following Matlab project contains the source code and Matlab examples used for core conceptual optimization of rotorcraft environment. CORE was written to facilitate optimization and design space exploration in the conceptual design phase or rotorcraft.

The source code and files included in this project are listed in the project files section, please make sure whether the listed source code meet your needs there.

Project Files: 

File NameSize
ACbuilder.m 1879
betafinder.m 1069
CMATpick_point.m 1205
CMATplot_the_carpet.m 6386
COREchooseproject.m 1892
COREmainmenu.m 1498
COREmkrequirements.m 6364
core_help.html 96174
CORE_ITERATE.m 4209
EVALnonlcons.m 1384
EVALobjective.m 848
IGEvi.m 437
ITERevaluate_X0.m 1398
ITERfix_decision_variables.m 1384
ITERmake_CON_MAT.m 5290
ITERmodify_composite_obj.m 978
ITERmodify_constraints.m 2293
ITERmodify_LB_X0_UB.m 1546
ITERoptimoptset.m 1909
ITERrun_optimizer.m 6272
ITERsave_hist.m 3903
loadfactor.m 425
moga.jpg 40776
PAblade_elements.m 4601
PointAnalysisBEA.m 6406
PointAnalysisMOM.m 4598
PointAnalysisMOM_assumptions.m 128
Requirements_template.xls 35328
retreating_stall_envelope.m 1109
SELECTind_from_pop.m 5856
simpleTRsizing.m 769
tail_rotor_power.m 478
about utilities.txt 328
convarea.m 1349
convmass.m 642
convpower.m 1860
convtime.m 5124
convvel.m 817
cosspace.m 1369
g0.m 463
get_yes_or_no.m 1943
lininterp1f.m 339
linspace3.m 1527
optimize.m 41753
progressbar.m 12126
sinspace.m 1191
stdatmo.m 10494
txtmenu.m 4366
vis.jpg 47491
vLdistribution.m 626
bpolar_simple.m 2686
constraint_BladeAR.m 355
constraint_Dlength.m 393
demo.setup.mat 1183
fusepolar_arealoading.m 400
History.xls 29184
Obj_max_W_P.m 814
Obj_min_AUM.m 765
plapse_simple.m 3183
Requirements.xls 35840
twistf_linear.m 416
weightestimate_baseline.m 3097
wingpolar_simple.m 753
Run_CORE.m 3265
bpolar_0012.m 7446
bpolar_simple.m 2686
constraint_BladeAR.m 355
constraint_Dlength.m 393
fusepolar_arealoading.m 400
Obj_max_W_P.m 814
Obj_min_AUM.m 765
Obj_min_size.m 796
plapse_simple.m 3213
twistf_linear.m 416
weightestimate_baseline.m 3097
weightestimate_decVar.m 502
wingpolar_simple.m 753
license.txt 1489

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