void WingGeom::UpdateDrawObj()
{
Geom::UpdateDrawObj();
Matrix4d attachMat;
Matrix4d relTrans;
attachMat = ComposeAttachMatrix();
relTrans = attachMat;
relTrans.affineInverse();
relTrans.matMult( m_ModelMatrix.data() );
relTrans.postMult( attachMat.data() );
int nxsec = m_XSecSurf.NumXSec();
m_XSecDrawObj_vec.resize( nxsec, DrawObj() );
//==== Tesselate Surface ====//
for ( int i = 0 ; i < nxsec ; i++ )
{
m_XSecDrawObj_vec[i].m_PntVec = m_XSecSurf.FindXSec( i )->GetDrawLines( m_TessW(), relTrans );
m_XSecDrawObj_vec[i].m_GeomChanged = true;
}
m_HighlightXSecDrawObj.m_PntVec = m_XSecSurf.FindXSec( m_ActiveAirfoil )->GetDrawLines( m_TessW(), relTrans );
m_HighlightXSecDrawObj.m_GeomChanged = true;
double w = m_XSecSurf.FindXSec( m_ActiveAirfoil )->GetXSecCurve()->GetWidth();
Matrix4d mat;
m_XSecSurf.GetBasicTransformation( Z_DIR, X_DIR, XS_SHIFT_MID, false, 1.0, mat );
mat.scale( 1.0/w );
VspCurve crv = m_XSecSurf.FindXSec( m_ActiveAirfoil )->GetUntransformedCurve();
crv.Transform( mat );
vector< vec3d > pts;
crv.Tesselate( m_TessW(), pts );
m_CurrentXSecDrawObj.m_PntVec = pts;
m_CurrentXSecDrawObj.m_LineWidth = 1.0;
m_CurrentXSecDrawObj.m_LineColor = vec3d( 0.0, 0.0, 0.0 );
m_CurrentXSecDrawObj.m_Type = DrawObj::VSP_LINES;
m_CurrentXSecDrawObj.m_GeomChanged = true;
VspCurve inbd = m_XSecSurf.FindXSec( m_ActiveXSec - 1 )->GetCurve();
inbd.Transform( relTrans );
VspCurve outbd = m_XSecSurf.FindXSec( m_ActiveXSec )->GetCurve();
outbd.Transform( relTrans );
BndBox iBBox, oBBox;
inbd.GetBoundingBox( iBBox );
outbd.GetBoundingBox( oBBox );
oBBox.Update( iBBox );
m_HighlightWingSecDrawObj.m_PntVec = oBBox.GetBBoxDrawLines();
}
string PropGeom::BuildBEMResults()
{
// Calculate prop center and normal vector
vec3d cen = m_ModelMatrix.xform( vec3d( 0, 0, 0 ) );
vec3d norm = m_ModelMatrix.xform( vec3d( -1.0, 0, 0 ) ) - cen;
int n = m_TessU();
//==== Create Results ====//
Results* res = ResultsMgr.CreateResults( "PropBEM" );
res->Add( NameValData( "Num_Sections", n ) );
res->Add( NameValData( "Num_Blade", m_Nblade() ) );
res->Add( NameValData( "Diameter", m_Diameter() ) );
res->Add( NameValData( "Beta34", m_Beta34() ) );
res->Add( NameValData( "Feather", m_Feather() ) );
res->Add( NameValData( "Center", cen ) );
res->Add( NameValData( "Normal", norm ) );
double rfirst = m_ChordCurve.GetRFirst();
double rlast = m_ChordCurve.GetRLast();
// Establish points to evaluate sections at.
vector < double > vtess;
m_MainSurfVec[0].MakeVTess( m_TessW(), vtess, m_CapUMinTess(), false );
vector < double > r_vec(n);
vector < double > chord_vec(n);
vector < double > twist_vec(n);
vector < double > rake_vec(n);
vector < double > skew_vec(n);
double rspan = rlast - rfirst;
for ( int i = 0; i < n; i++ )
{
double t = static_cast < double > ( i ) / ( n - 1 );
double r = rfirst + rspan * Cluster( t, m_RootCluster(), m_TipCluster() );
double u = m_rtou.CompPnt( r );
VspCurve c;
m_FoilSurf.GetUConstCurve( c, u );
vec3d v = c.CompPnt( 0 );
c.OffsetZ( -v.z() );
vector < vec3d > pts;
c.Tesselate( vtess, pts );
vector < double > xpts( pts.size() );
vector < double > ypts( pts.size() );
for ( int j = 0; j < pts.size(); j++ )
{
xpts[j] = pts[j].x();
ypts[j] = pts[j].y();
}
char str[255];
sprintf( str, "%03d", i );
res->Add( NameValData( "XSection_" + string( str ), xpts ) );
res->Add( NameValData( "YSection_" + string( str ), ypts ) );
r_vec[i] = r;
chord_vec[i] = m_ChordCurve.Comp( r );
twist_vec[i] = m_TwistCurve.Comp( r );
rake_vec[i] = m_RakeCurve.Comp( r );
skew_vec[i] = m_SkewCurve.Comp( r );
}
res->Add( NameValData( "Radius", r_vec ) );
res->Add( NameValData( "Chord", chord_vec ) );
res->Add( NameValData( "Twist", twist_vec ) );
res->Add( NameValData( "Rake", rake_vec ) );
res->Add( NameValData( "Skew", skew_vec ) );
return res->GetID();
}
