应用介绍

免费下载用于复合叶片分析和设计的软件的matlab代码

%% clear all variables and close files/figures

clear all;

close('all');

fclose('all');

format compact;

%% set the Co-Blade version

SIM.version = '1.20.00-dcs';

%% add paths to the source code

SIM.rootDir     = pwd; 

SIM.sourceDir   = [SIM.rootDir filesep 'Source'];

SIM.airfoilDir  = [SIM.rootDir filesep 'Airfoil_Data'];

SIM.materialDir = [SIM.rootDir filesep 'Material_Data'];

SIM.laminateDir = [SIM.rootDir filesep 'Laminate_Data'];

SIM.optimDir    = [SIM.rootDir filesep 'Optimization_Data'];

% NOTE: comment out the addpath commands before compiling

addpath( SIM.sourceDir )

addpath([SIM.sourceDir filesep 'consolidator'])

addpath([SIM.sourceDir filesep 'dispCorrectionFactor'])

addpath([SIM.sourceDir filesep 'export_fig'])

addpath([SIM.sourceDir filesep 'polygeom'])

addpath([SIM.sourceDir filesep 'psopt'])

%% set debugging breakpoints

% dbstop in structOptimize.m at 453

% dbstop in structAnalysis.m at 332

%% Read the list of active input files

fid = fopen([SIM.rootDir filesep 'Active_Input_Files.inp'], 'r');

if fid == -1

    error(['ERROR: Could not locate and open file ' [SIM.rootDir filesep 'Active_Input_Files.inp']]);

end

inpList = textscan(fid,'%s');

fclose(fid);

SIM.inpFile = inpList{:};

nInpFiles   = numel(SIM.inpFile);

SIM.case    = cell(nInpFiles, 1);

for iSIM = 1:nInpFiles

    [pathstr SIM.case{iSIM} ext] = fileparts(SIM.inpFile{iSIM});

end

%% main loop that sequentially executes the active input files

for iSIM = 1:nInpFiles 

    fprintf(1, 'Executing case %s with Co-Blade v%s.\n', SIM.inpFile{iSIM}, SIM.version);

    clear ANLS OPT ENV BLADE WEB OUT MATS AF Coord % clear data structures from previous input files (don't want to accidentally keep any old values)

         [ANLS OPT ENV BLADE WEB OUT MATS AF Coord] = CoBlade_init(iSIM, SIM); 

    %% Define the laminate data, either by optimization, or read data from the laminate input files

    if OPT.OPTIMIZE

        WEB.inbStn = OPT.INB_STN .* ones(WEB.NUM_WEBS, 1);  % all the webs begin and end at blade stations INB_STN and OUB_STN

        WEB.oubStn = OPT.OUB_STN .* ones(WEB.NUM_WEBS, 1);

        % Determine the laminate data from optimization routine

        [WEB SECNODES LamData] = structOptimize(iSIM, SIM, ANLS, OPT, ENV, BLADE, WEB, AF, MATS, Coord, OUT);

    else

        % Read the pre-defined laminate data from the laminate input files

        [SECNODES LamData] = readLaminateData(SIM, BLADE, WEB, MATS);

    end

    %% execute the structural analysis

    [Panel StrProps AppLoads ResLoads Disp NormS ShearS Buckle MidPlane LaminaSS Modes] ...

     = structAnalysis(iSIM, SIM, ANLS, ENV, BLADE, WEB, MATS, LamData, AF, SECNODES, Coord);

    %% write output files

    if OPT.OPTIMIZE || OPT.OPT_PITAXIS

        % create a copy of the main input file, but update any parameters that were changed/created by the optimization routine                 

        if OPT.OPTIMIZE

            BLADE.strFile = cell(BLADE.NUM_SEC, 1); % overwrite this variable with the new names

            for n = 1:BLADE.NUM_SEC

                BLADE.strFile{n} = [SIM.case{iSIM} '_OPT_' num2str(n) '.lam'];

            end 

        end

        writeInpFileNewMain(iSIM, SIM, OPT, BLADE, WEB);

    end

    if OUT.PROPS_FILE

        writeOupFileProps(iSIM, SIM, BLADE, StrProps, OUT);

    end   

    if OUT.LOAD_DSP_FILE

        writeOupFileLoads(iSIM, SIM, BLADE, AppLoads, ResLoads, Disp, OUT);

    end

    if OUT.PANEL_FILE

        writeOupFilePanel(iSIM, SIM, BLADE, WEB, SECNODES, Panel, NormS, ShearS, Buckle, OUT);

    end

    if OUT.LAMINA_FILE

        writeOupFileLamina(iSIM, SIM, BLADE, WEB, SECNODES, Panel, Buckle, LaminaSS, OUT);

    end

    %% create output plots

    if OUT.DATA_GUI

        startDataGUI(iSIM, SIM, OPT, BLADE, WEB, AF, Panel, LaminaSS);

    end

    if OUT.PLOT_F_BLD || OUT.PLOT_DISP_BLD

        plotLoadsDisp(iSIM, SIM, BLADE, AF, Coord, AppLoads, Disp, StrProps, OUT)

    end

    if OUT.PLOT_YMOD

        plotBladeYModulus(iSIM, SIM, BLADE, WEB, OUT, Panel)

    end

    if OUT.PLOT_GMOD

        plotBladeGModulus(iSIM, SIM, BLADE, WEB, OUT, Panel)

    end

    if OUT.PLOT_MASS_DEN || OUT.PLOT_PRIN_ANG || OUT.PLOT_AT_STFF || ...

       OUT.PLOT_BSTFF    || OUT.PLOT_INER     || OUT.PLOT_CENTERS

        plotStructProps(iSIM, SIM, BLADE, StrProps, OUT);

    end

    if OUT.PLOT_NORMS

        plotBladeNormStress(iSIM, SIM, BLADE, WEB, OUT, Panel, NormS)

    end

    if OUT.PLOT_SHEARS

        plotBladeShearStress(iSIM, SIM, BLADE, WEB, OUT, Panel, ShearS)

    end

    if OUT.PLOT_BCRIT

        plotBladeBuckleCrit(iSIM, SIM, BLADE, WEB, OUT, Panel, Buckle)

    end

    if OUT.PLOT_E11 || OUT.PLOT_E22 || OUT.PLOT_E12

        plotLaminaStrain(iSIM, SIM, BLADE, WEB, MATS, Panel, LaminaSS, OUT)

    end

    if OUT.PLOT_S11 || OUT.PLOT_S22 || OUT.PLOT_S12

        plotLaminaStress(iSIM, SIM, BLADE, WEB, MATS, Panel, LaminaSS, OUT)

    end

    if OUT.PLOT_S11_FC || OUT.PLOT_S22_FC || OUT.PLOT_S12_FC

        plotLaminaStressFC(iSIM, SIM, BLADE, WEB, MATS, Panel, LaminaSS, OUT)

    end

    if ( OUT.PLOT_MODE_S || OUT.PLOT_MODE_D ) && ANLS.N_MODES >= 1

        plotModes(iSIM, SIM, ANLS, Modes, OUT)

    end

    if OUT.PLOT_APPLOADS || OUT.PLOT_RESLOADS

        plotLoads(iSIM, SIM, BLADE, AppLoads, ResLoads, OUT)

    end

    if OUT.PLOT_DEFLECT

        plotDeflect(iSIM, SIM, BLADE, Disp, OUT)

    end

    fprintf(1, 'Co-Blade v%s terminated normally for case %s. \r\n', SIM.version, SIM.inpFile{iSIM});

end % for iSIM = 1:nInpFiles