//==== Drag Parameters ====//
void StackGeom::LoadDragFactors( DragFactors& drag_factors )
{
double max_xsec_area = 0.000000000001;
for ( int i = 0 ; i < ( int )m_XSecSurf.NumXSec() ; i++ )
{
XSec* xs = m_XSecSurf.FindXSec( i );
XSecCurve* xsc = xs->GetXSecCurve();
double a = xsc->ComputeArea( );
if ( a > max_xsec_area )
{
max_xsec_area = a;
}
}
// drag_factors.m_Length = m_Length();
drag_factors.m_MaxXSecArea = max_xsec_area;
// drag_factors.m_LengthToDia = m_Length() / dia;
}
//==== Update Fuselage And Cross Section Placement ====//
void PropGeom::UpdateSurf()
{
int nxsec = m_XSecSurf.NumXSec();
double radius = m_Diameter() / 2.0;
double rfirst = 0.0;
double rlast = 1.0;
vector < double > uvec( nxsec );
vector < double > rvec( nxsec );
double rev = 1.0;
if ( m_ReverseFlag() )
{
rev = -1.0;
}
//==== Update XSec Location/Rotation ====//
for ( int i = 0 ; i < nxsec ; i++ )
{
PropXSec* xs = ( PropXSec* ) m_XSecSurf.FindXSec( i );
if ( xs )
{
if ( xs->GetXSecCurve()->GetType() == XS_POINT )
{
printf( "Warning: XS_POINT type not valid for propellers\n" );
// Propellers are constructed in two phases. The first phase stacks
// all the XSecs with unit chord. Intermediate curves are extracted
// from that surface and are scaled to match the required chord.
// Since XS_POINT XSecs already have zero chord, they mess up this
// process.
}
//==== Reset Group Names ====//
xs->SetGroupDisplaySuffix( i );
//==== Set X Limits ====//
EnforceOrder( xs, i );
xs->SetRefLength( radius );
bool first = false;
bool last = false;
if( i == 0 ) first = true;
else if( i == (nxsec-1) ) last = true;
if ( first )
{
rfirst = xs->m_RadiusFrac();
}
if ( last )
{
rlast = xs->m_RadiusFrac();
}
uvec[i] = i;
rvec[i] = xs->m_RadiusFrac();
}
}
m_rtou = Vsp1DCurve();
m_rtou.InterpolateLinear( uvec, rvec, false );
EnforcePCurveOrder( rfirst, rlast );
// Set lower limit for activity factor integration limit
m_AFLimit.SetLowerLimit( rfirst );
// Integrate activity factor.
m_AF.Set( m_ChordCurve.IntegrateAF( m_AFLimit() ) );
m_AF.Deactivate();
if ( m_UseBeta34Flag() == 1 )
{
if ( rfirst <= 0.75 )
{
double theta34 = m_TwistCurve.Comp( 0.75 );
m_Feather = m_Beta34() - theta34;
}
else
{
m_Feather = m_Beta34();
}
m_Beta34.Activate();
m_Feather.Deactivate();
}
else
{
if ( rfirst <= 0.75 )
{
double theta34 = m_TwistCurve.Comp( 0.75 );
m_Beta34 = m_Feather() + theta34;
}
else
{
m_Beta34 = m_Feather();
}
m_Beta34.Deactivate();
m_Feather.Activate();
}
// Set up fold axis & store for visualization.
Matrix4d fold, foldrot;
fold.loadIdentity();
fold.rotateY( m_AzimuthFoldDir() );
fold.rotateX( m_ElevationFoldDir() );
m_FoldAxDirection = fold.xform( vec3d( 0, 0, 1 ) );
m_FoldAxOrigin = vec3d( m_AxialFoldAxis() * radius, m_RadFoldAxis() * radius, m_OffsetFoldAxis() * radius );
//==== Cross Section Curves & joint info ====//
vector< VspCurve > crv_vec;
crv_vec.resize( nxsec );
//==== Update XSec Location/Rotation ====//
for ( int i = 0 ; i < nxsec ; i++ )
{
PropXSec* xs = ( PropXSec* ) m_XSecSurf.FindXSec( i );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
double r = xs->m_RadiusFrac();
double w = m_ChordCurve.Comp( r ) * radius;
if ( xsc )
{
//==== Find Width Parm ====//
string width_id = xsc->GetWidthParmID();
Parm* width_parm = ParmMgr.FindParm( width_id );
piecewise_curve_type pwc;
if ( width_parm )
{
width_parm->Deactivate();
Airfoil* af = dynamic_cast < Airfoil* > ( xsc );
if ( af )
{
width_parm->Set( 1.0 );
xs->GetXSecCurve()->SetFakeWidth( w );
xs->GetXSecCurve()->SetUseFakeWidth( true );
pwc = xs->GetCurve().GetCurve();
xs->GetXSecCurve()->SetUseFakeWidth( false );
width_parm->Set( w );
}
else
{
CircleXSec* cir = dynamic_cast < CircleXSec* > ( xsc );
if ( cir )
{
width_parm->Set( 1.0 );
pwc = xs->GetCurve().GetCurve();
width_parm->Set( w );
}
else
{
double h = xs->GetXSecCurve()->GetHeight();
xsc->SetWidthHeight( 1.0, h/w );
pwc = xs->GetCurve().GetCurve();
xsc->SetWidthHeight( w, h );
}
}
}
else
{
pwc = xs->GetCurve().GetCurve();
}
// Set up prop positioner for highlight curves - not lofting.
xs->m_PropPos.m_ParentProp = GetXSecSurf( 0 );
xs->m_PropPos.m_Radius = r * radius;
xs->m_PropPos.m_Chord = w;
xs->m_PropPos.m_Twist = m_TwistCurve.Comp( r );
xs->m_PropPos.m_XRotate = 0.0;
xs->m_PropPos.m_ZRotate = atan( -m_RakeCurve.Compdt( r ) ) * 180.0 / PI;
xs->m_PropPos.m_Rake = m_RakeCurve.Comp( r ) * radius;
xs->m_PropPos.m_Skew = m_SkewCurve.Comp( r ) * radius;
xs->m_PropPos.m_PropRot = m_Rotate();
xs->m_PropPos.m_Feather = m_Feather();
xs->m_PropPos.m_FoldOrigin = m_FoldAxOrigin;
xs->m_PropPos.m_FoldDirection = m_FoldAxDirection;
xs->m_PropPos.m_FoldAngle = m_FoldAngle();
xs->m_PropPos.m_Reverse = rev;
crv_vec[i].SetCurve( pwc );
}
}
}
// This surface linearly interpolates the airfoil sections without
// any other transformations.
// These sections can be extracted (as u-const curves) and then
// transformed to their final position before skinning.
m_FoilSurf = VspSurf();
m_FoilSurf.SkinC0( crv_vec, false );
// Find the union of stations required to approximate the blade parameters
// with cubic functions.
vector < double > tmap = rvec; // Initialize with specified XSecs.
vector < double > tdisc;
tdisc.push_back( rfirst );
tdisc.push_back( rlast );
for ( int i = 0; i < m_pcurve_vec.size(); i++ )
{
vector < double > tm;
vector < double > tmout;
vector < double > td;
m_pcurve_vec[i]->GetTMap( tm, td );
std::set_union( tmap.begin(), tmap.end(), tm.begin(), tm.end(), std::back_inserter(tmout), &aboutcomp );
std::swap( tmout, tmap );
}
// Not sure why above set_union leaves duplicate entries, but
// sort and force unique just to be sure.
std::sort( tmap.begin(), tmap.end() );
auto tmit = std::unique( tmap.begin(), tmap.end(), &abouteq );
tmap.erase( tmit, tmap.end() );
// Treat all control points as possible discontinuities.
tdisc = tmap;
// Refine by adding two intermediate points to each cubic section
// this is needed because the adaptive algorithm above uses derivatives
// while our later reconstruction does not.
vector < double > tref( ( tmap.size() - 1 ) * 3 + 1 );
for ( int i = 0; i < tmap.size() - 1; i++ )
{
int iref = 3*i;
double t = tmap[i];
double tnxt = tmap[i+1];
double dt = (tnxt-t)/3.0;
tref[iref] = t;
tref[iref+1] = t + dt;
tref[iref+2] = t + 2 * dt;
}
tref.back() = tmap.back();
std::swap( tmap, tref );
// Convert tdisc to final parameterization.
for ( int i = 0; i < tdisc.size(); i++ )
{
tdisc[i] = ( tdisc[i] - rfirst ) / ( rlast - rfirst );
}
// Pseudo cross sections
// Not directly user-controlled, but an intermediate step in lofting the
// surface.
int npseudo = tmap.size();
vector < rib_data_type > rib_vec( npseudo );
vector < double > u_pseudo( npseudo );
for ( int i = 0; i < npseudo; i++ )
{
// Assume linear interpolation means linear u/r relationship.
double r = tmap[i];
double u = m_rtou.CompPnt( r );
VspCurve c;
m_FoilSurf.GetUConstCurve( c, u );
vec3d v = c.CompPnt( 0 );
c.OffsetZ( -v.z() );
PropPositioner pp;
pp.m_ParentProp = this->GetXSecSurf( 0 );
pp.m_Radius = r * radius;
pp.m_Chord = m_ChordCurve.Comp( r ) * radius;
pp.m_Twist = m_TwistCurve.Comp( r );
pp.m_XRotate = 0.0;
pp.m_ZRotate = atan( -m_RakeCurve.Compdt( r ) ) * 180.0 / PI;
pp.m_Rake = m_RakeCurve.Comp( r ) * radius;
pp.m_Skew = m_SkewCurve.Comp( r ) * radius;
pp.m_PropRot = m_Rotate();
pp.m_Feather = m_Feather();
pp.m_FoldOrigin = m_FoldAxOrigin;
pp.m_FoldDirection = m_FoldAxDirection;
pp.m_FoldAngle = m_FoldAngle();
pp.m_Reverse = rev;
// Set a bunch of other pp variables.
pp.SetCurve( c );
pp.Update();
rib_vec[i].set_f( pp.GetCurve().GetCurve() );
u_pseudo[i] = ( r - rfirst ) / ( rlast - rfirst );
}
m_MainSurfVec.resize( 1 );
m_MainSurfVec.reserve( m_Nblade() );
m_MainSurfVec[0].SetMagicVParm( false );
m_MainSurfVec[0].SkinCubicSpline( rib_vec, u_pseudo, tdisc, false );
m_MainSurfVec[0].SetMagicVParm( true );
m_MainSurfVec[0].SetSurfType( PROP_SURF );
m_MainSurfVec[0].SetClustering( m_LECluster(), m_TECluster() );
m_MainSurfVec[0].SetFoilSurf( &m_FoilSurf );
if ( m_XSecSurf.GetFlipUD() )
{
m_MainSurfVec[0].FlipNormal();
}
if ( this->m_ReverseFlag() )
{
m_MainSurfVec[0].FlipNormal();
}
// UpdateEndCaps here so we only have to cap one blade.
UpdateEndCaps();
m_MainSurfVec.resize( m_Nblade(), m_MainSurfVec[0] );
// Duplicate capping variables
m_CapUMinSuccess.resize( m_Nblade(), m_CapUMinSuccess[0] );
m_CapUMaxSuccess.resize( m_Nblade(), m_CapUMaxSuccess[0] );
m_CapWMinSuccess.resize( m_Nblade(), m_CapWMinSuccess[0] );
m_CapWMaxSuccess.resize( m_Nblade(), m_CapWMaxSuccess[0] );
Matrix4d rot;
for ( int i = 1; i < m_Nblade(); i++ )
{
double theta = 360.0 * i / ( double )m_Nblade();
rot.loadIdentity();
rot.rotateX( theta );
m_MainSurfVec[i].Transform( rot );
}
CalculateMeshMetrics( u_pseudo );
}
void FuselageScreen::GuiDeviceCallBack( GuiDevice* gui_device )
{
//==== Find Fuselage Ptr ====//
Geom* geom_ptr = m_ScreenMgr->GetCurrGeom();
if ( !geom_ptr || geom_ptr->GetType().m_Type != FUSELAGE_GEOM_TYPE )
{
return;
}
FuselageGeom* fuselage_ptr = dynamic_cast< FuselageGeom* >( geom_ptr );
assert( fuselage_ptr );
if ( gui_device == &m_XSecIndexSelector )
{
fuselage_ptr->SetActiveXSecIndex( m_XSecIndexSelector.GetIndex() );
fuselage_ptr->Update();
}
else if ( gui_device == &m_XSecTypeChoice )
{
int t = m_XSecTypeChoice.GetVal();
fuselage_ptr->SetActiveXSecType( t );
}
else if ( gui_device == &m_ShowXSecButton )
{
m_ScreenMgr->ShowScreen( ScreenMgr::VSP_XSEC_SCREEN );
}
else if ( gui_device == &m_CutXSec )
{
fuselage_ptr->CutActiveXSec();
}
else if ( gui_device == &m_CopyXSec )
{
fuselage_ptr->CopyActiveXSec();
}
else if ( gui_device == &m_PasteXSec )
{
fuselage_ptr->PasteActiveXSec();
}
else if ( gui_device == &m_InsertXSec )
{
fuselage_ptr->InsertXSec( );
}
else if ( gui_device == &m_ReadFuseFileButton )
{
int xsid = fuselage_ptr->GetActiveXSecIndex();
XSec* xs = fuselage_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_FILE_FUSE )
{
FileXSec* file_xs = dynamic_cast< FileXSec* >( xsc );
assert( file_xs );
string newfile = m_ScreenMgr->GetSelectFileScreen()->FileChooser( "Fuselage Cross Section", "*.fxs" );
file_xs->ReadXsecFile( newfile );
file_xs->Update();
xs->Update();
fuselage_ptr->Update();
}
}
}
}
else if ( gui_device == &m_AfReadFileButton )
{
int xsid = fuselage_ptr->GetActiveXSecIndex();
XSec* xs = fuselage_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_FILE_AIRFOIL )
{
FileAirfoil* affile_xs = dynamic_cast< FileAirfoil* >( xsc );
assert( affile_xs );
string newfile = m_ScreenMgr->GetSelectFileScreen()->FileChooser( "Airfoil File", "*.{af,dat}", false );
affile_xs->ReadFile( newfile );
affile_xs->Update();
xs->Update();
fuselage_ptr->Update();
}
}
}
}
else if ( gui_device == &m_DesignPolicyChoice )
{
// This is a hack to get the XSecXSlider to update its ranges. This
// requires setting the ID to another valid FractionParm's ID. In this
// case, m_YLocPercent of the same XSec. It will get set back to
// m_XLocPercent in Update() before anyone notices the change.
int xsid = fuselage_ptr->GetActiveXSecIndex();
FuseXSec* xs = (FuseXSec*) fuselage_ptr->GetXSec( xsid );
if ( xs )
{
m_XSecXSlider.Update( xs->m_YLocPercent.GetID() );
}
}
SkinScreen::GuiDeviceCallBack( gui_device );
}
//==== Update Pod Screen ====//
bool FuselageScreen::Update()
{
assert( m_ScreenMgr );
Geom* geom_ptr = m_ScreenMgr->GetCurrGeom();
if ( !geom_ptr || geom_ptr->GetType().m_Type != FUSELAGE_GEOM_TYPE )
{
Hide();
return false;
}
SkinScreen::Update();
m_NumUSlider.Deactivate();
FuselageGeom* fuselage_ptr = dynamic_cast< FuselageGeom* >( geom_ptr );
assert( fuselage_ptr );
//==== Design ====//
m_LengthSlider.Update( fuselage_ptr->m_Length.GetID() );
m_DesignPolicyChoice.Update( fuselage_ptr->m_OrderPolicy.GetID() );
//==== Skin & XSec Index Display ===//
int xsid = fuselage_ptr->GetActiveXSecIndex();
m_XSecIndexSelector.SetIndex( xsid );
FuseXSec* xs = ( FuseXSec* ) fuselage_ptr->GetXSec( xsid );
if ( xs )
{
bool firstxs = xsid == 0;
bool lastxs = xsid == ( fuselage_ptr->GetXSecSurf( 0 )->NumXSec() - 1 );
//==== XSec ====//
m_SectUTessSlider.Update( xs->m_SectTessU.GetID() );
if ( firstxs )
{
m_SectUTessSlider.Deactivate();
}
m_XSecXSlider.Update( xs->m_XLocPercent.GetID() );
m_XSecYSlider.Update( xs->m_YLocPercent.GetID() );
m_XSecZSlider.Update( xs->m_ZLocPercent.GetID() );
m_XSecXRotSlider.Update( xs->m_XRotate.GetID() );
m_XSecYRotSlider.Update( xs->m_YRotate.GetID() );
m_XSecZRotSlider.Update( xs->m_ZRotate.GetID() );
m_XSecSpinSlider.Update( xs->m_Spin.GetID() );
if ( firstxs && ( fuselage_ptr->m_OrderPolicy() == FuselageGeom::FUSE_MONOTONIC || fuselage_ptr->m_OrderPolicy() == FuselageGeom::FUSE_LOOP ) )
{
m_XSecXSlider.Deactivate();
}
if ( lastxs && fuselage_ptr->m_OrderPolicy() == FuselageGeom::FUSE_MONOTONIC )
{
m_XSecXSlider.Deactivate();
}
if ( lastxs && fuselage_ptr->m_OrderPolicy() == FuselageGeom::FUSE_LOOP )
{
m_XSecXSlider.Deactivate();
m_XSecYSlider.Deactivate();
m_XSecZSlider.Deactivate();
m_XSecXRotSlider.Deactivate();
m_XSecYRotSlider.Deactivate();
m_XSecZRotSlider.Deactivate();
m_XSecSpinSlider.Deactivate();
}
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
m_XSecTypeChoice.SetVal( xsc->GetType() );
if ( lastxs && fuselage_ptr->m_OrderPolicy() == FuselageGeom::FUSE_LOOP )
{
m_XSecTypeChoice.Deactivate();
}
else
{
m_XSecTypeChoice.Activate();
}
if ( lastxs && fuselage_ptr->m_OrderPolicy() == FuselageGeom::FUSE_LOOP )
{
DisplayGroup ( NULL);
}
else if ( xsc->GetType() == XS_POINT )
{
DisplayGroup( NULL );
}
else if ( xsc->GetType() == XS_SUPER_ELLIPSE )
{
DisplayGroup( &m_SuperGroup );
SuperXSec* super_xs = dynamic_cast< SuperXSec* >( xsc );
assert( super_xs );
m_SuperHeightSlider.Update( super_xs->m_Height.GetID() );
m_SuperWidthSlider.Update( super_xs->m_Width.GetID() );
m_SuperMSlider.Update( super_xs->m_M.GetID() );
m_SuperNSlider.Update( super_xs->m_N.GetID() );
}
else if ( xsc->GetType() == XS_CIRCLE )
{
DisplayGroup( &m_CircleGroup );
CircleXSec* circle_xs = dynamic_cast< CircleXSec* >( xsc );
assert( circle_xs );
m_DiameterSlider.Update( circle_xs->m_Diameter.GetID() );
}
else if ( xsc->GetType() == XS_ELLIPSE )
{
DisplayGroup( & m_EllipseGroup );
EllipseXSec* ellipse_xs = dynamic_cast< EllipseXSec* >( xsc );
m_EllipseHeightSlider.Update( ellipse_xs->m_Height.GetID() );
m_EllipseWidthSlider.Update( ellipse_xs->m_Width.GetID() );
}
else if ( xsc->GetType() == XS_ROUNDED_RECTANGLE )
{
DisplayGroup( & m_RoundedRectGroup );
RoundedRectXSec* rect_xs = dynamic_cast< RoundedRectXSec* >( xsc );
assert( rect_xs );
m_RRHeightSlider.Update( rect_xs->m_Height.GetID() );
m_RRWidthSlider.Update( rect_xs->m_Width.GetID() );
m_RRRadiusSlider.Update( rect_xs->m_Radius.GetID() );
}
else if ( xsc->GetType() == XS_GENERAL_FUSE )
{
DisplayGroup( &m_GenGroup );
GeneralFuseXSec* gen_xs = dynamic_cast< GeneralFuseXSec* >( xsc );
assert( gen_xs );
m_GenHeightSlider.Update( gen_xs->m_Height.GetID() );
m_GenWidthSlider.Update( gen_xs->m_Width.GetID() );
m_GenMaxWidthLocSlider.Update( gen_xs->m_MaxWidthLoc.GetID() );
m_GenCornerRadSlider.Update( gen_xs->m_CornerRad.GetID() );
m_GenTopTanAngleSlider.Update( gen_xs->m_TopTanAngle.GetID() );
m_GenBotTanAngleSlider.Update( gen_xs->m_BotTanAngle.GetID() );
m_GenTopStrSlider.Update( gen_xs->m_TopStr.GetID() );
m_GenBotStrSlider.Update( gen_xs->m_BotStr.GetID() );
m_GenUpStrSlider.Update( gen_xs->m_UpStr.GetID() );
m_GenLowStrSlider.Update( gen_xs->m_LowStr.GetID() );
}
else if ( xsc->GetType() == XS_FOUR_SERIES )
{
DisplayGroup( &m_FourSeriesGroup );
FourSeries* fs_xs = dynamic_cast< FourSeries* >( xsc );
assert( fs_xs );
m_FourChordSlider.Update( fs_xs->m_Chord.GetID() );
m_FourThickChordSlider.Update( fs_xs->m_ThickChord.GetID() );
m_FourCamberSlider.Update( fs_xs->m_Camber.GetID() );
m_FourCamberLocSlider.Update( fs_xs->m_CamberLoc.GetID() );
m_FourInvertButton.Update( fs_xs->m_Invert.GetID() );
m_FourNameOutput.Update( fs_xs->GetAirfoilName() );
}
else if ( xsc->GetType() == XS_SIX_SERIES )
{
DisplayGroup( &m_SixSeriesGroup );
SixSeries* ss_xs = dynamic_cast< SixSeries* >( xsc );
assert( ss_xs );
m_SixChordSlider.Update( ss_xs->m_Chord.GetID() );
m_SixThickChordSlider.Update( ss_xs->m_ThickChord.GetID() );
m_SixIdealClSlider.Update( ss_xs->m_IdealCl.GetID() );
m_SixASlider.Update( ss_xs->m_A.GetID() );
m_SixInvertButton.Update( ss_xs->m_Invert.GetID() );
m_SixNameOutput.Update( ss_xs->GetAirfoilName() );
m_SixSeriesChoice.Update( ss_xs->m_Series.GetID() );
}
else if ( xsc->GetType() == XS_BICONVEX )
{
DisplayGroup( &m_BiconvexGroup );
Biconvex* bi_xs = dynamic_cast< Biconvex* >( xsc );
assert( bi_xs );
m_BiconvexChordSlider.Update( bi_xs->m_Chord.GetID() );
m_BiconvexThickChordSlider.Update( bi_xs->m_ThickChord.GetID() );
}
else if ( xsc->GetType() == XS_WEDGE )
{
DisplayGroup( &m_WedgeGroup );
Wedge* we_xs = dynamic_cast< Wedge* >( xsc );
assert( we_xs );
m_WedgeChordSlider.Update( we_xs->m_Chord.GetID() );
m_WedgeThickChordSlider.Update( we_xs->m_ThickChord.GetID() );
m_WedgeThickLocSlider.Update( we_xs->m_ThickLoc.GetID() );
}
else if ( xsc->GetType() == XS_FILE_FUSE )
{
DisplayGroup( &m_FuseFileGroup );
FileXSec* file_xs = dynamic_cast< FileXSec* >( xsc );
assert( file_xs );
m_FileHeightSlider.Update( file_xs->m_Height.GetID() );
m_FileWidthSlider.Update( file_xs->m_Width.GetID() );
}
else if ( xsc->GetType() == XS_FILE_AIRFOIL )
{
DisplayGroup( &m_AfFileGroup );
FileAirfoil* affile_xs = dynamic_cast< FileAirfoil* >( xsc );
assert( affile_xs );
m_AfFileChordSlider.Update( affile_xs->m_Chord.GetID() );
m_AfFileInvertButton.Update( affile_xs->m_Invert.GetID() );
m_AfFileNameOutput.Update( affile_xs->GetAirfoilName() );
}
}
}
return true;
}
void WingScreen::GuiDeviceCallBack( GuiDevice* gui_device )
{
//==== Find Fuselage Ptr ====//
Geom* geom_ptr = m_ScreenMgr->GetCurrGeom();
if ( !geom_ptr || geom_ptr->GetType().m_Type != MS_WING_GEOM_TYPE )
{
return;
}
WingGeom* wing_ptr = dynamic_cast< WingGeom* >( geom_ptr );
assert( wing_ptr );
if ( gui_device == &m_AfIndexSelector )
{
wing_ptr->SetActiveAirfoilIndex( m_AfIndexSelector.GetIndex() );
wing_ptr->Update();
}
else if ( gui_device == &m_AfModIndexSelector )
{
wing_ptr->SetActiveAirfoilIndex( m_AfModIndexSelector.GetIndex() );
wing_ptr->Update();
}
else if ( gui_device == &m_SectIndexSelector )
{
wing_ptr->SetActiveXSecIndex( m_SectIndexSelector.GetIndex() );
wing_ptr->Update();
}
else if ( gui_device == &m_SplitSectButton )
{
int wsid = wing_ptr->GetActiveXSecIndex();
wing_ptr->SplitWingSect( wsid );
wing_ptr->Update();
}
else if ( gui_device == &m_CutSectButton )
{
int wsid = wing_ptr->GetActiveXSecIndex();
wing_ptr->CutWingSect( wsid );
wing_ptr->Update();
}
else if ( gui_device == &m_CopySectButton )
{
int wsid = wing_ptr->GetActiveXSecIndex();
wing_ptr->CopyWingSect( wsid );
wing_ptr->Update();
}
else if ( gui_device == &m_PasteSectButton )
{
int wsid = wing_ptr->GetActiveXSecIndex();
wing_ptr->PasteWingSect( wsid );
wing_ptr->Update();
}
else if ( gui_device == &m_InsertSectButton )
{
int wsid = wing_ptr->GetActiveXSecIndex();
wing_ptr->InsertWingSect( wsid );
wing_ptr->Update();
}
else if ( gui_device == &m_AfTypeChoice )
{
int t = m_AfTypeChoice.GetVal();
wing_ptr->SetActiveAirfoilType( t );
wing_ptr->Update();
}
else if ( gui_device == &m_ShowXSecButton )
{
m_ScreenMgr->ShowScreen( ScreenMgr::VSP_XSEC_SCREEN );
}
else if ( gui_device == &m_CopyAfButton )
{
int afid = wing_ptr->GetActiveAirfoilIndex();
wing_ptr->CopyAirfoil( afid );
}
else if ( gui_device == &m_PasteAfButton )
{
int afid = wing_ptr->GetActiveAirfoilIndex();
wing_ptr->PasteAirfoil(afid);
wing_ptr->Update();
}
else if ( gui_device == &m_ReadFuseFileButton )
{
int xsid = wing_ptr->GetActiveAirfoilIndex();
XSec* xs = wing_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_FILE_FUSE )
{
FileXSec* file_xs = dynamic_cast< FileXSec* >( xsc );
assert( file_xs );
string newfile = m_ScreenMgr->GetSelectFileScreen()->FileChooser( "Fuselage Cross Section", "*.fxs" );
file_xs->ReadXsecFile( newfile );
file_xs->Update();
xs->Update();
wing_ptr->Update();
}
}
}
}
else if ( gui_device == &m_AfReadFileButton )
{
int xsid = wing_ptr->GetActiveAirfoilIndex();
XSec* xs = wing_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_FILE_AIRFOIL )
{
FileAirfoil* affile_xs = dynamic_cast< FileAirfoil* >( xsc );
assert( affile_xs );
string newfile = m_ScreenMgr->GetSelectFileScreen()->FileChooser( "Airfoil File", "*.{af,dat}", false );
affile_xs->ReadFile( newfile );
affile_xs->Update();
xs->Update();
wing_ptr->Update();
}
}
}
}
else if ( gui_device == &m_UpPromoteButton )
{
int xsid = wing_ptr->GetActiveAirfoilIndex();
XSec* xs = wing_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_CST_AIRFOIL )
{
CSTAirfoil* cst_xs = dynamic_cast< CSTAirfoil* >( xsc );
assert( cst_xs );
cst_xs->PromoteUpper();
cst_xs->Update();
xs->Update();
wing_ptr->Update();
}
}
}
}
else if ( gui_device == &m_LowPromoteButton )
{
int xsid = wing_ptr->GetActiveAirfoilIndex();
XSec* xs = wing_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_CST_AIRFOIL )
{
CSTAirfoil* cst_xs = dynamic_cast< CSTAirfoil* >( xsc );
assert( cst_xs );
cst_xs->PromoteLower();
cst_xs->Update();
xs->Update();
wing_ptr->Update();
}
}
}
}
else if ( gui_device == &m_UpDemoteButton )
{
int xsid = wing_ptr->GetActiveAirfoilIndex();
XSec* xs = wing_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_CST_AIRFOIL )
{
CSTAirfoil* cst_xs = dynamic_cast< CSTAirfoil* >( xsc );
assert( cst_xs );
cst_xs->DemoteUpper();
cst_xs->Update();
xs->Update();
wing_ptr->Update();
}
}
}
}
else if ( gui_device == &m_LowDemoteButton )
{
int xsid = wing_ptr->GetActiveAirfoilIndex();
XSec* xs = wing_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_CST_AIRFOIL )
{
CSTAirfoil* cst_xs = dynamic_cast< CSTAirfoil* >( xsc );
assert( cst_xs );
cst_xs->DemoteLower();
cst_xs->Update();
xs->Update();
wing_ptr->Update();
}
}
}
}
else if ( ( gui_device == &m_FourFitCSTButton ) ||
( gui_device == &m_SixFitCSTButton ) ||
( gui_device == &m_AfFileFitCSTButton ) )
{
int xsid = wing_ptr->GetActiveAirfoilIndex();
XSec* xs = wing_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
Airfoil* af_xs = dynamic_cast< Airfoil* >( xsc );
if ( af_xs )
{
VspCurve c = af_xs->GetOrigCurve();
int deg = af_xs->m_FitDegree();
wing_ptr->SetActiveAirfoilType( XS_CST_AIRFOIL );
XSec* newxs = wing_ptr->GetXSec( xsid );
if ( newxs )
{
XSecCurve* newxsc = newxs->GetXSecCurve();
if ( newxsc )
{
if ( newxsc->GetType() == XS_CST_AIRFOIL )
{
CSTAirfoil* cst_xs = dynamic_cast< CSTAirfoil* >( newxsc );
assert( cst_xs );
cst_xs->FitCurve( c, deg );
cst_xs->Update();
newxs->Update();
wing_ptr->Update();
}
}
}
}
}
}
}
else if ( gui_device == &m_TestDriverGroupButton )
{
int wsid = wing_ptr->GetActiveXSecIndex();
WingSect* wing_sect = dynamic_cast<WingSect*>(wing_ptr->GetXSec( wsid ));
if ( wing_sect )
{
vector< string > parm_ids = wing_sect->GetDriverParms();
wing_sect->m_DriverGroup.Test( parm_ids, 1e-4 );
}
}
GeomScreen::GuiDeviceCallBack( gui_device );
}
//==== Update Wing Screen ====//
bool WingScreen::Update()
{
assert( m_ScreenMgr );
char str[256];
Geom* geom_ptr = m_ScreenMgr->GetCurrGeom();
if ( !geom_ptr || geom_ptr->GetType().m_Type != MS_WING_GEOM_TYPE )
{
Hide();
return false;
}
GeomScreen::Update();
m_NumUSlider.Deactivate();
WingGeom* wing_ptr = dynamic_cast< WingGeom* >( geom_ptr );
assert( wing_ptr );
//==== Plan Parms ===//
m_PlanSpanSlider.Update( wing_ptr->m_TotalSpan.GetID() );
m_PlanProjSpanSlider.Update( wing_ptr->m_TotalProjSpan.GetID() );
m_PlanChordSlider.Update( wing_ptr->m_TotalChord.GetID() );
m_PlanAreaSlider.Update( wing_ptr->m_TotalArea.GetID() );
m_LEClusterSlider.Update( wing_ptr->m_LECluster.GetID() );
m_TEClusterSlider.Update( wing_ptr->m_TECluster.GetID() );
sprintf( str, "%6.4f", wing_ptr->m_TotalProjSpan() * wing_ptr->m_TotalProjSpan() / wing_ptr->m_TotalArea() );
m_PlanAROutput.Update( str );
m_RootCapTypeChoice.Update( wing_ptr->m_CapUMinOption.GetID() );
m_TipCapTypeChoice.Update( wing_ptr->m_CapUMaxOption.GetID() );
if ( wing_ptr->m_CapUMinOption() == VspSurf::NO_END_CAP &&
wing_ptr->m_CapUMaxOption() == VspSurf::NO_END_CAP )
{
m_CapTessSlider.Deactivate();
}
else
{
m_CapTessSlider.Update( wing_ptr->m_CapUMinTess.GetID() );
}
WingSect* root_sect = dynamic_cast<WingSect*>(wing_ptr->GetXSec( 0 ));
if ( root_sect )
{
m_IncidenceSlider.Update( root_sect->m_Twist.GetID() );
m_IncidenceLocSlider.Update( root_sect->m_TwistLoc.GetID() );
}
sprintf( str, " %d", wing_ptr->NumXSec()-1 );
m_NumSectOutput.Update( str );
////==== Wing Section Index Display ====//
int ws_index = wing_ptr->GetActiveXSecIndex();
m_SectIndexSelector.SetIndex( ws_index );
WingSect* wing_sect = dynamic_cast<WingSect*>(wing_ptr->GetXSec( ws_index ));
if ( wing_sect )
{
m_SectUTessSlider.Update( wing_sect->m_SectTessU.GetID() );
m_RootClusterSlider.Update( wing_sect->m_RootCluster.GetID() );
m_TipClusterSlider.Update( wing_sect->m_TipCluster.GetID() );
m_WingDriverGroupBank.SetDriverGroup( &wing_sect->m_DriverGroup );
vector< string > parm_ids = wing_sect->GetDriverParms();
wing_sect->m_DriverGroup.UpdateGroup( parm_ids );
m_WingDriverGroupBank.Update( parm_ids );
m_SweepSlider.Update( wing_sect->m_Sweep.GetID() );
m_SweepLocSlider.Update( wing_sect->m_SweepLoc.GetID() );
m_SecSweepLocSlider.Update( wing_sect->m_SecSweepLoc.GetID() );
m_TwistSlider.Update( wing_sect->m_Twist.GetID() );
m_TwistLocSlider.Update( wing_sect->m_TwistLoc.GetID() );
m_DihedralSlider.Update( wing_sect->m_Dihedral.GetID() );
m_DihedralAbsRelToggle.Update( wing_ptr->m_RelativeDihedralFlag.GetID() );
m_TwistAbsRelToggle.Update( wing_ptr->m_RelativeTwistFlag.GetID() );
m_RotateFoilMatchDihedral.Update( wing_ptr->m_RotateAirfoilMatchDiedralFlag.GetID() );
sprintf( str, " %6.4f", wing_sect->GetProjectedSpan() );
m_SectProjSpanOutput.Update( str );
}
//==== XSec Index Display ===//
int xsid = wing_ptr->GetActiveAirfoilIndex();
m_AfIndexSelector.SetIndex( xsid );
m_AfModIndexSelector.SetIndex( xsid );
WingSect* ws = ( WingSect* ) wing_ptr->GetXSec( xsid );
if ( ws )
{
XSecCurve* xsc = ws->GetXSecCurve();
if ( xsc )
{
m_AfTypeChoice.SetVal( xsc->GetType() );
if ( xsc->GetType() == XS_POINT )
{
DisplayGroup( NULL );
}
else if ( xsc->GetType() == XS_SUPER_ELLIPSE )
{
DisplayGroup( &m_SuperGroup );
SuperXSec* super_xs = dynamic_cast< SuperXSec* >( xsc );
assert( super_xs );
m_SuperHeightSlider.Update( super_xs->m_Height.GetID() );
m_SuperWidthSlider.Update( super_xs->m_Width.GetID() );
m_SuperMSlider.Update( super_xs->m_M.GetID() );
m_SuperNSlider.Update( super_xs->m_N.GetID() );
}
else if ( xsc->GetType() == XS_CIRCLE )
{
DisplayGroup( &m_CircleGroup );
CircleXSec* circle_xs = dynamic_cast< CircleXSec* >( xsc );
assert( circle_xs );
m_DiameterSlider.Update( circle_xs->m_Diameter.GetID() );
}
else if ( xsc->GetType() == XS_ELLIPSE )
{
DisplayGroup( & m_EllipseGroup );
EllipseXSec* ellipse_xs = dynamic_cast< EllipseXSec* >( xsc );
m_EllipseHeightSlider.Update( ellipse_xs->m_Height.GetID() );
m_EllipseWidthSlider.Update( ellipse_xs->m_Width.GetID() );
}
else if ( xsc->GetType() == XS_ROUNDED_RECTANGLE )
{
DisplayGroup( & m_RoundedRectGroup );
RoundedRectXSec* rect_xs = dynamic_cast< RoundedRectXSec* >( xsc );
assert( rect_xs );
m_RRHeightSlider.Update( rect_xs->m_Height.GetID() );
m_RRWidthSlider.Update( rect_xs->m_Width.GetID() );
m_RRRadiusSlider.Update( rect_xs->m_Radius.GetID() );
}
else if ( xsc->GetType() == XS_GENERAL_FUSE )
{
DisplayGroup( &m_GenGroup );
GeneralFuseXSec* gen_xs = dynamic_cast< GeneralFuseXSec* >( xsc );
assert( gen_xs );
m_GenHeightSlider.Update( gen_xs->m_Height.GetID() );
m_GenWidthSlider.Update( gen_xs->m_Width.GetID() );
m_GenMaxWidthLocSlider.Update( gen_xs->m_MaxWidthLoc.GetID() );
m_GenCornerRadSlider.Update( gen_xs->m_CornerRad.GetID() );
m_GenTopTanAngleSlider.Update( gen_xs->m_TopTanAngle.GetID() );
m_GenBotTanAngleSlider.Update( gen_xs->m_BotTanAngle.GetID() );
m_GenTopStrSlider.Update( gen_xs->m_TopStr.GetID() );
m_GenBotStrSlider.Update( gen_xs->m_BotStr.GetID() );
m_GenUpStrSlider.Update( gen_xs->m_UpStr.GetID() );
m_GenLowStrSlider.Update( gen_xs->m_LowStr.GetID() );
}
else if ( xsc->GetType() == XS_FOUR_SERIES )
{
DisplayGroup( &m_FourSeriesGroup );
FourSeries* fs_xs = dynamic_cast< FourSeries* >( xsc );
assert( fs_xs );
m_FourChordSlider.Update( fs_xs->m_Chord.GetID() );
m_FourThickChordSlider.Update( fs_xs->m_ThickChord.GetID() );
m_FourCamberSlider.Update( fs_xs->m_Camber.GetID() );
m_FourCamberLocSlider.Update( fs_xs->m_CamberLoc.GetID() );
m_FourInvertButton.Update( fs_xs->m_Invert.GetID() );
m_FourNameOutput.Update( fs_xs->GetAirfoilName() );
m_FourDegreeCounter.Update( fs_xs->m_FitDegree.GetID() );
m_FourEqArcLenButton.Update( fs_xs->m_EqArcLen.GetID() );
}
else if ( xsc->GetType() == XS_SIX_SERIES )
{
DisplayGroup( &m_SixSeriesGroup );
SixSeries* ss_xs = dynamic_cast< SixSeries* >( xsc );
assert( ss_xs );
m_SixChordSlider.Update( ss_xs->m_Chord.GetID() );
m_SixThickChordSlider.Update( ss_xs->m_ThickChord.GetID() );
m_SixIdealClSlider.Update( ss_xs->m_IdealCl.GetID() );
m_SixASlider.Update( ss_xs->m_A.GetID() );
m_SixInvertButton.Update( ss_xs->m_Invert.GetID() );
m_SixNameOutput.Update( ss_xs->GetAirfoilName() );
m_SixSeriesChoice.Update( ss_xs->m_Series.GetID() );
m_SixDegreeCounter.Update( ss_xs->m_FitDegree.GetID() );
}
else if ( xsc->GetType() == XS_BICONVEX )
{
DisplayGroup( &m_BiconvexGroup );
Biconvex* bi_xs = dynamic_cast< Biconvex* >( xsc );
assert( bi_xs );
m_BiconvexChordSlider.Update( bi_xs->m_Chord.GetID() );
m_BiconvexThickChordSlider.Update( bi_xs->m_ThickChord.GetID() );
}
else if ( xsc->GetType() == XS_WEDGE )
{
DisplayGroup( &m_WedgeGroup );
Wedge* we_xs = dynamic_cast< Wedge* >( xsc );
assert( we_xs );
m_WedgeChordSlider.Update( we_xs->m_Chord.GetID() );
m_WedgeThickChordSlider.Update( we_xs->m_ThickChord.GetID() );
m_WedgeThickLocSlider.Update( we_xs->m_ThickLoc.GetID() );
}
else if ( xsc->GetType() == XS_FILE_FUSE )
{
DisplayGroup( &m_FuseFileGroup );
FileXSec* file_xs = dynamic_cast< FileXSec* >( xsc );
assert( file_xs );
m_FileHeightSlider.Update( file_xs->m_Height.GetID() );
m_FileWidthSlider.Update( file_xs->m_Width.GetID() );
}
else if ( xsc->GetType() == XS_FILE_AIRFOIL )
{
DisplayGroup( &m_AfFileGroup );
FileAirfoil* affile_xs = dynamic_cast< FileAirfoil* >( xsc );
assert( affile_xs );
m_AfFileChordSlider.Update( affile_xs->m_Chord.GetID() );
m_AfFileInvertButton.Update( affile_xs->m_Invert.GetID() );
m_AfFileNameOutput.Update( affile_xs->GetAirfoilName() );
m_AfFileDegreeCounter.Update( affile_xs->m_FitDegree.GetID() );
}
else if ( xsc->GetType() == XS_CST_AIRFOIL )
{
DisplayGroup( &m_CSTAirfoilGroup );
CSTAirfoil* cst_xs = dynamic_cast< CSTAirfoil* >( xsc );
assert( cst_xs );
int num_up = cst_xs->m_UpDeg() + 1;
int num_low = cst_xs->m_LowDeg() + 1;
char str[255];
sprintf( str, "%d", cst_xs->m_UpDeg() );
m_UpDegreeOutput.Update( str );
sprintf( str, "%d", cst_xs->m_LowDeg() );
m_LowDegreeOutput.Update( str );
m_CSTInvertButton.Update( cst_xs->m_Invert.GetID() );
m_CSTContLERadButton.Update( cst_xs->m_ContLERad.GetID() );
m_CSTEqArcLenButton.Update( cst_xs->m_EqArcLen.GetID() );
if ( ( m_UpCoeffSliderVec.size() != num_up ) || ( m_LowCoeffSliderVec.size() != num_low ) )
{
RebuildCSTGroup( cst_xs );
}
for ( int i = 0; i < num_up; i++ )
{
Parm *p = cst_xs->m_UpCoeffParmVec[i];
if ( p )
{
m_UpCoeffSliderVec[i].Update( p->GetID() );
}
}
for ( int i = 0; i < num_low; i++ )
{
Parm *p = cst_xs->m_LowCoeffParmVec[i];
if ( p )
{
m_LowCoeffSliderVec[i].Update( p->GetID() );
}
}
if ( cst_xs->m_ContLERad() && num_low > 0 )
{
m_LowCoeffSliderVec[0].Deactivate();
}
}
m_TECloseChoice.Update( xsc->m_TECloseType.GetID() );
m_TECloseGroup.Update( xsc->m_TECloseAbsRel.GetID() );
m_CloseThickSlider.Update( xsc->m_TECloseThick.GetID() );
m_CloseThickChordSlider.Update( xsc->m_TECloseThickChord.GetID() );
if ( xsc->m_TECloseType() != CLOSE_NONE )
{
m_TECloseABSButton.Activate();
m_TECloseRELButton.Activate();
if ( xsc->m_TECloseAbsRel() == ABS )
{
m_CloseThickSlider.Activate();
m_CloseThickChordSlider.Deactivate();
}
else
{
m_CloseThickSlider.Deactivate();
m_CloseThickChordSlider.Activate();
}
}
else
{
m_CloseThickSlider.Deactivate();
m_CloseThickChordSlider.Deactivate();
m_TECloseABSButton.Deactivate();
m_TECloseRELButton.Deactivate();
}
m_TETrimChoice.Update( xsc->m_TETrimType.GetID() );
m_TETrimGroup.Update( xsc->m_TETrimAbsRel.GetID() );
m_TrimXSlider.Update( xsc->m_TETrimX.GetID() );
m_TrimXChordSlider.Update( xsc->m_TETrimXChord.GetID() );
m_TrimThickSlider.Update( xsc->m_TETrimThick.GetID() );
m_TrimThickChordSlider.Update( xsc->m_TETrimThickChord.GetID() );
m_TrimXSlider.Deactivate();
m_TrimXChordSlider.Deactivate();
m_TrimThickSlider.Deactivate();
m_TrimThickChordSlider.Deactivate();
m_TETrimABSButton.Deactivate();
m_TETrimRELButton.Deactivate();
if ( xsc->m_TETrimType() != TRIM_NONE )
{
m_TETrimABSButton.Activate();
m_TETrimRELButton.Activate();
}
if ( xsc->m_TETrimType() == TRIM_X )
{
if ( xsc->m_TETrimAbsRel() == ABS )
{
m_TrimXSlider.Activate();
}
else
{
m_TrimXChordSlider.Activate();
}
}
else if ( xsc->m_TETrimType() == TRIM_THICK )
{
if ( xsc->m_TETrimAbsRel() == ABS )
{
m_TrimThickSlider.Activate();
}
else
{
m_TrimThickChordSlider.Activate();
}
}
m_AFThetaSlider.Update( xsc->m_Theta.GetID() );
m_AFScaleSlider.Update( xsc->m_Scale.GetID() );
m_AFDeltaXSlider.Update( xsc->m_DeltaX.GetID() );
m_AFDeltaYSlider.Update( xsc->m_DeltaY.GetID() );
m_AFShiftLESlider.Update( xsc->m_ShiftLE.GetID() );
}
}
return true;
}
void StackScreen::GuiDeviceCallBack( GuiDevice* gui_device )
{
//==== Find Fuselage Ptr ====//
Geom* geom_ptr = m_ScreenMgr->GetCurrGeom();
if ( !geom_ptr || geom_ptr->GetType().m_Type != STACK_GEOM_TYPE )
{
return;
}
StackGeom* stackgeom_ptr = dynamic_cast< StackGeom* >( geom_ptr );
assert( stackgeom_ptr );
if ( gui_device == &m_XSecIndexSelector )
{
stackgeom_ptr->SetActiveXSecIndex( m_XSecIndexSelector.GetIndex() );
stackgeom_ptr->Update();
}
else if ( gui_device == &m_XSecTypeChoice )
{
int t = m_XSecTypeChoice.GetVal();
stackgeom_ptr->SetActiveXSecType( t );
}
else if ( gui_device == &m_ShowXSecButton )
{
m_ScreenMgr->ShowScreen( ScreenMgr::VSP_XSEC_SCREEN );
}
else if ( gui_device == &m_CutXSec )
{
stackgeom_ptr->CutActiveXSec();
}
else if ( gui_device == &m_CopyXSec )
{
stackgeom_ptr->CopyActiveXSec();
}
else if ( gui_device == &m_PasteXSec )
{
stackgeom_ptr->PasteActiveXSec();
}
else if ( gui_device == &m_InsertXSec )
{
stackgeom_ptr->InsertXSec( );
}
else if ( gui_device == &m_ReadFuseFileButton )
{
int xsid = stackgeom_ptr->GetActiveXSecIndex();
XSec* xs = stackgeom_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_FILE_FUSE )
{
FileXSec* file_xs = dynamic_cast< FileXSec* >( xsc );
assert( file_xs );
string newfile = m_ScreenMgr->GetSelectFileScreen()->FileChooser( "Fuselage Cross Section", "*.fxs" );
file_xs->ReadXsecFile( newfile );
file_xs->Update();
xs->Update();
stackgeom_ptr->Update();
}
}
}
}
else if ( gui_device == &m_AfReadFileButton )
{
int xsid = stackgeom_ptr->GetActiveXSecIndex();
XSec* xs = stackgeom_ptr->GetXSec( xsid );
if ( xs )
{
XSecCurve* xsc = xs->GetXSecCurve();
if ( xsc )
{
if ( xsc->GetType() == XS_FILE_AIRFOIL )
{
FileAirfoil* affile_xs = dynamic_cast< FileAirfoil* >( xsc );
assert( affile_xs );
string newfile = m_ScreenMgr->GetSelectFileScreen()->FileChooser( "Airfoil File", "*.{af,dat}" );
affile_xs->ReadFile( newfile );
affile_xs->Update();
xs->Update();
stackgeom_ptr->Update();
}
}
}
}
SkinScreen::GuiDeviceCallBack( gui_device );
}