float Ship::Wm(){
float c1, c2;
c1 = c2 = 0.;
float PdV = Pd(v.Vk)/Vol();
float c3 = pow(v.Year, 0.4) - 19;
if (PdV > 40)
c1 = 0.14 * c3;
else if (PdV > 26)
c1 = 0.13 * c3;
else if (PdV > 21)
c1 = 0.21 * c3;
else if (PdV > 10)
c1 = 0.22 * c3;
else c1 = 1.;
if (Vol() > 5000)
c1 = 1.;
if (v.Year < 1915)
c2 = 1.9;
else if(v.Year < 1933)
c2 = 1.6;
else c2 = 0.92;
return find(et, e.Eng).K1 * pow(Pd(v.Vk), find(et, e.Eng).K2)* (pow((pow(v.Year, 0.45) - 29.3), 2.) + 0.45) * c1 * c2 * find(st, e.Gear).Wgear;
}
void CIndicator::Render(std::vector<struct kline_struct>* pvData)
{
m_pvData = pvData;
if (!m_pRender)
return;
m_pRender->BeginRender(m_rcArea);
if (m_nIndicatorType == INDICATOR_TYPE_MA)
{
KLine();
}
else if (m_nIndicatorType == INDICATOR_TYPE_VOL)
{
Vol();
}
else
{
CColorUtil clr(0, 0, 255);
m_pRender->DrawRectangle(m_rcMemDC, clr);
m_pRender->DrawText(m_rcMemDC, _T("macd"), clr);
}
m_pRender->EndRender();
}
params::params(char *address)
{
//read data from input file
std::ifstream param(address);
std::ostringstream param_trimmed_out;
std::string input_line;
while (!param.eof())
{
std::getline(param,input_line);
if ((int(input_line[0])!=0)&&(int(input_line[0])!=35)) param_trimmed_out<<input_line<<std::endl;
}
param.close();
std::istringstream param_trimmed_in(param_trimmed_out.str());
param_trimmed_in>>IsBox_;
param_trimmed_in>>Nx_tot_>>Ny_tot_>>Nz_tot_;
param_trimmed_in>>Lx_>>Ly_>>Lz_;
param_trimmed_in>>bs_;
param_trimmed_in>>Np_track_;
param_trimmed_in>>T_final_>>dt_>>threshold_;
param_trimmed_in>>Statistics_>>Stat_print_;
param_trimmed_in>>Data_freq_fast_>>Data_freq_slow_;
param_trimmed_in>>Data_dir_>>Stat_dir_;
param_trimmed_in>>Initial_;
param_trimmed_in>>PreCond_>>Solver_;
param_trimmed_in>>cooling_;
param_trimmed_in>>Iteration1_>>Iteration2_>>epsilon_;
param_trimmed_in>>TWC_>>ParticleGravity_;
param_trimmed_in>>A1_>>A2_;
param_trimmed_in>>Rho0_;
param_trimmed_in>>U0_;
param_trimmed_in>>T0_;
param_trimmed_in>>Mu0_>>k_;
param_trimmed_in>>gx1_>>gy1_>>gz1_>>gx2_>>gy2_>>gz2_;
param_trimmed_in>>Cp_>>Cv_;
param_trimmed_in>>np0_;
param_trimmed_in>>Dp_>>Rhop_;
param_trimmed_in>>Cvp_;
param_trimmed_in>>epsilonp_;
param_trimmed_in>>Nu_;
param_trimmed_in>>I01_>>I02_;
//initially update parameters
R_ = Cp_ - Cv_;
P0_ = Rho0_ * T0_ * R_;
Tp_ = Rhop_ * Dp_ * Dp_ / ( 18 * Mu0_ );
mp_ = Rhop_ * PI * Dp_ * Dp_ * Dp_ / 6.;
W_ = Ly_;
N0_ = (int)(np0_*Vol());
Iteration_ = Iteration1_;
A_ = A1_;
gx_ = gx1_;
gy_ = gy1_;
gz_ = gz1_;
I0_ = I01_;
}
float Ship::Bunker(){
float b1 = v.Range / (1. + 0.4 * v.Coalpct);
float b2 = 0.;
float b3 = 1.8/Pd(v.Vc) * v.Range * v.Vc * 0.1;
if (v.Year < 1898 || e.Eng == QuadExp || e.Eng == TripExp)
b2 = 1. - (1910 - v.Year)/70.;
else if (v.Year < 1920)
b2 = 1. + (v.Year - 1910)/20.;
else if( v.Year < 1950)
b2 = 1.5 + (v.Year - 1920)/60.;
else
b2 = 2 + (v.Year - 1950)/60.;
float c1 = (Pd(v.Vk)/Vol() > 15 && Pd(v.Vk)/Vol() < 18) ? 0.3 : 1;
return (b1 / (b2 * b3) + 0.005 * Vol()) * c1 * find(et, e.Eng).FcE * find(st, e.Gear).FcT;
}
float Ship::t(){
float M = v.Lpp / pow(Vol(), 1./3.);
int Fa;
switch(e.Faa){
case N: Fa = 0; break;
case U: Fa = -2; break;
case V: Fa = 2; break;
default: Fa = 0;
}
float BL = v.B / v.Lpp;
float d = 0.625 * BL + 0.08;
float e = 0.165 - 0.25 * BL;
float f = 525. - 8060. * BL + 20300. * pow(BL, 2.);
float t1 = d + e / (f * pow(0.98 - Cb(), 3.) + 1.);
float t2 = -0.01 * Fa;
float t3 = 2. * (Dprop()/v.Lpp - 0.04);
return t1 + t2 + t3 - 0.26 + 0.04 * M;
}
float Ship::w(){
float M = v.Lpp / pow(Vol(), 1./3.);
int Fa;
switch(e.Faa){
case N: Fa = 0; break;
case U: Fa = -2; break;
case V: Fa = 2; break;
default: Fa = 0;
}
float BL = v.B / v.Lpp;
float a = 0.1 * BL + 0.149;
float b = 0.05 * BL + 0.449;
float c = 585. - 5027. * BL + 11700. * pow(BL, 2.);
float w1 = a + b / (c * pow(0.98 - Cb(), 3.) + 1);
float w2 = 0.025 * Fa / (100. * pow(Cb() - 0.7, 2.) + 1);
float w3 = min(0.1, -0.18 + 0.00756 / (Dprop()/v.Lpp + 0.002));
float S1 = e.Shafts > 1 ? 1. : 0.7;
return 0.7 * (w1 + w2 + w3) - 0.45 + 0.08 * M * S1;
}
float Ship::Flotation(){
float c1 = Stability() > 1 ? sqrt(Stability()) : pow(Stability(), 4.);
float c4 = v.Year < 1850 ? 0.4 : (v.Year > 1890 ? 1 : 1 - 3. * (1890 - v.Year) / 200.);
return (WPA() / 35. + Vol()) / 2. * c1 * c4;
}
void Ship::output(){
ofstream file;
file.open("Report.txt");
file << "[table]" << endl;
cout << fixed << setprecision(2) << "Length: \t\t\t\t" << v.Lpp << " m" << endl;
file << fixed << setprecision(2) << "[tr][td]Length: \t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t[/td][td]" << v.Lpp << " m[/td][/tr]" << endl;
cout << "Beam: \t\t\t\t\t" << v.B << " m" << endl;
file << "[tr][td]Beam: [/td][td]" << v.B << " m[/td][/tr]" << endl;
cout << "Draft: \t\t\t\t\t" << v.D << " m" << endl;
file << "[tr][td]Draft: [/td][td]" << v.D << " m[/td][/tr]" << endl;
cout << "Freeboard: \t\t\t\t" << v.fB << " m" << endl;
file << "[tr][td]Freeboard: [/td][td]" << v.fB << " m[/td][/tr]" << endl;
cout << setprecision(3) << "Block Coefficient: \t\t\t" << Cb() << endl;
file << setprecision(3) << "[tr][td]Block Coefficient: [/td][td]" << Cb() << "[/td][/tr]" << endl;
cout << setprecision(0) << "Displacement: \t\t\t\t" << Vol() << " t" << endl;
file << setprecision(0) << "[tr][td]Displacement: [/td][td]" << Vol() << " t[/td][/tr]" << endl;
cout << "Lightship: \t\t\t\t" << Wh() + Wwo() + Wm() + We() + Wspus() + Bunker() << " t" << endl;
file << "[tr][td]Lightship: [/td][td]" << Lightship() << " t[/td][/tr]" << endl;
cout << setprecision(1) << "\nMax Speed: \t\t\t\t" << v.Vk << " kn" << endl;
file << setprecision(1) << "\n[tr][td]Max Speed: [/td][td]" << v.Vk << " kn[/td][/tr]" << endl;
cout << "Cruise Speed: \t\t\t\t" << v.Vc << " kn / " << v.Range << " nm" << endl;
file << "[tr][td]Cruise Speed: [/td][td]" << v.Vc << " kn / " << v.Range << " nm[/td][/tr]" << endl;
cout << "Engine: \t\t\t\t";
file << "[tr][td]Engine: [/td][td]";
switch(e.Gear){
case Direct:
cout << "Direct ";
file << "Direct ";
break;
case Geared:
cout << "Geared ";
file << "Geared ";
break;
case Turbo_Electric:
cout << "Turbo-Electric ";
file << "Turbo-Electric ";
break;
default:
cout << "Unknown";
file << "Unknown";
}
switch(e.Eng){
case Diesel2stk:
cout << "Two Stroke Diesel" << endl;
file << "Two Stroke Diesel";
break;
case Diesel4stk:
cout << "Four Stroke Diesel" << endl;
file << "Four Stroke Diesel" << endl;
break;
case QuadExp:
cout << "Quadruple Expansion Reciprocating Engine" << endl;
file << "Quadruple Expansion Reciprocating Engine";
break;
case TripExp:
cout << "Triple Expansion Reciprocating Engine" << endl;
file << "Triple Expansion Reciprocating Engine";
break;
case SimExp:
cout << "Simple Reciprocating Engine" << endl;
file << "Simple Reciprocating Engine";
break;
case SteamTur:
cout << "Steam Turbine" << endl;
file << "Steam Turbine";
break;
default:
cout << endl;
}
file << "[/td][/tr]" << endl;
cout << setprecision(0) << "Power Delivered: \t\t\t" << Pd(v.Vk) << " hp" << endl;
file << setprecision(0) << "[tr][td]Power Delivered: [/td][td]" << Pd(v.Vk) << " hp[/td][/tr]" << endl;
cout << setprecision(2) << "Total Efficiency: \t\t\t" << NUt()*100 << "%" << endl;
file << setprecision(2) << "[tr][td]Total Efficiency: [/td][td]" << NUt()*100 << "%[/td][/tr]" << endl;
cout << setprecision(3) << "Froude Number: \t\t\t\t" << Fn() << endl;
file << setprecision(3) << "[tr][td]Froude Number: [/td][td]" << Fn() << "[/td][/tr]" << endl;
cout << setprecision(0) << "Bunker Size: \t\t\t\t" << Bunker() << " t" << endl;
file << setprecision(0) << "[tr][td]Bunker Size: [/td][td]" << Bunker() << " t[/td][/tr]" << endl;
cout << "Service Allowance: \t\t\t" << e.SA << "%" << endl;
file << "[tr][td]Service Allowance: [/td][td]" << e.SA << "%[/td][/tr]" << endl;
cout << setprecision(2);
file << setprecision(2);
cout << "Length of Superstructure: \t\t" << v.Lspus << " m" << endl;
file << "[tr][td]Length of Superstructure: [/td][td]" << v.Lspus << " m[/td][/tr]" << endl;
cout << "Aftbody Shape: \t\t\t\t";
file << "[tr][td]Aftbody Shape: [/td][td]";
switch(e.Faa){
case V:
cout << "V" << endl;
file << "V";
break;
case U:
cout << "U" << endl;
file << "U";
break;
case N:
cout << "N" << endl;
file << "N";
break;
default:
cout << "N" << endl;
file << "N";
}
file << "[/td][/tr]";
cout << "\nLongitudinal Center of Buoyancy: \t" << lcb() << "%" << endl;
file << "\n[tr][td]Longitudinal Center of Buoyancy: [/td][td]" << lcb() << "% / " << lcb()*v.Lpp << " m from midpoint[/td][/tr]" << endl;
cout << "Longitudinal Center of Gravity: \t" << lcg() << "%" << endl;
file << "[tr][td]Longitudinal Center of Gravity: [/td][td]" << lcg() << "% / " << lcg()*v.Lpp << " m from midpoint[/td][/tr]" << endl;
cout << "Vertical Center of Gravity: \t\t" << KGh() << " m" << endl;
file << "[tr][td]Vertical Center of Gravity: [/td][td]" << KGh() << " m[/td][/tr]" << endl;
cout << "Metacentric Height: \t\t\t" << GM() << " m" << endl;
file << "[tr][td]Metacentric Height: [/td][td]" << GM() << " m[/td][/tr]" << endl;
cout << "Roll Period: \t\t\t\t" << TR() << " s" << endl;
file << "[tr][td]Roll Period: [/td][td]" << TR() << " s[/td][/tr]" << endl;
cout << "\nBow Entrance Angle: \t\t\t" << iE() << " deg" << endl;
file << "\n[tr][td]Bow Entrance Angle: [/td][td]" << iE() << " deg[/td][/tr]" << endl;
cout << "Length of Engine Room: \t\t\t" << Lcm() << " m" << endl;
file << "[tr][td]Length of Engine Room: [/td][td]" << Lcm() << " m[/td][/tr]" << endl;
cout << setprecision(0) << "\nMain Belt: \t\t\t\t" << arm.mb_Ttop << " / " << arm.mb_Tbot << " mm at " << arm.b_deg << " degrees, " << arm.b_L << " m long with " << arm.b_H << " m above and " << arm.b_Db << " m below water" << endl;
file << setprecision(0) << "\n[tr][td]Main Belt: [/td][td]" << arm.mb_Ttop << " / " << arm.mb_Tbot << " mm, " << arm.b_L << " m long with " << arm.b_H << " m above and " << arm.b_Db << " m below water[/td][/tr]" << endl;
cout << "End Belt: \t\t\t\t" << arm.eb_Ttop << " / " << arm.eb_Tbot << " mm" << endl;
file << "[tr][td]End Belt: [/td][td]" << arm.eb_Ttop << " / " << arm.eb_Tbot << " mm[/td][/tr]" << endl;
cout << "Upper Belt: \t\t\t\t" << arm.ub_Ttop << " / " << arm.ub_Tbot << " mm, " << arm.b_uL << " m long" << endl;
file << "[tr][td]Upper Belt: [/td][td]" << arm.ub_Ttop << " / " << arm.ub_Tbot << " mm, " << arm.b_uL << " m long[/td][/tr]" << endl;
cout << "Main Deck: \t\t\t\t" << arm.md_T << " mm covering " << arm.md_P << "% / " << arm.md_P * v.Lpp << " m of deck" << endl;
file << "[tr][td]Main Deck: [/td][td]" << arm.md_T << " m covering " << arm.md_P << "% / " << arm.md_P * v.Lpp << " m of deck[/td][/tr]" << endl;
cout << "Weather Deck: \t\t\t\t" << arm.wd_T << " mm covering " << arm.wd_P << "% / " << arm.wd_P * v.Lpp << " m of deck" << endl;
file << "[tr][td]Weather Deck: [/td][td]" << arm.wd_T << " m covering " << arm.wd_P << "% / " << arm.wd_P * v.Lpp << " m of deck[/td][/tr]" << endl;
cout << "Splinter Deck: \t\t\t\t" << arm.sd_T << " mm covering " << arm.sd_P << "% / " << arm.sd_P * v.Lpp << " m of deck" << endl;
file << "[tr][td]Splinter Deck: [/td][td]" << arm.sd_T << " m covering " << arm.sd_P << "% / " << arm.sd_P * v.Lpp << " m of deck[/td][/tr]" << endl;
cout << "Ends Deck: \t\t\t\t" << arm.ed_T << " mm" << endl;
file << "[tr][td]Ends Deck: [/td][td]" << arm.ed_T << " mm[/td][/tr]" << endl;
cout << "Bulkhead: \t\t\t\t" << arm.blk_T << " mm in " << arm.blk_Lct << "x" << arm.blk_D << " m layers, " << arm.blk_L << " m long, " << arm.blk_H << " m tall" << endl;
file << "[tr][td]Bulkhead: [/td][td]" << arm.blk_T << " mm in " << arm.blk_Lct << "x" << arm.blk_D << " m layers, " << arm.blk_L << " m long, " << arm.blk_H << " m tall[/td][/tr]" << endl;
file << "[/table]" << endl;
file.close();
}
float Ship::iE(){
float c1 = - pow(v.Lpp / v.B, 0.80856) * pow(1 - Cw(), 0.30484) * pow(1 - Cp() - 0.0225 * lcb(), 0.6367) * pow(lr() / v.B, 0.34574) * pow(100 * Vol() / pow(v.Lpp, 3.), 0.16302);
return 1 + 89 * exp(c1);
}
float Ship::Pe(float V){
return ( Sw()/sqrt(Vol() * v.Lpp) * pow(Vol(), 2./3.) * pow(V, 3.) /580.) * (1 + e.SA/100.);
}
float Ship::Sw(){
return 1.025 * 1.7 * v.Lpp * v.D + Vol()/v.D;
}
real total_torque_cpu () {
//<USER_DEFINED>
INPUT(Density);
real rplanet = sqrt(Xplanet*Xplanet+Yplanet*Yplanet+Zplanet*Zplanet);
real rsmoothing = THICKNESSSMOOTHING*ASPECTRATIO*pow(rplanet/R0,FLARINGINDEX)*rplanet;
//<\USER_DEFINED>
//<EXTERNAL>
real* dens = Density->field_cpu;
int pitch = Pitch_cpu;
int stride = Stride_cpu;
int size_x = Nx+2*NGHX;
int size_y = Ny+2*NGHY;
int size_z = Nz+2*NGHZ;
real rsm2 = rsmoothing*rsmoothing;
//<\EXTERNAL>
//<INTERNAL>
int i;
int j;
int k;
int ll;
real dx;
real dy;
real dz=0.0;
real InvDist3;
real cellmass;
real dist2;
real distance;
real fxi;
real fyi;
real tottorq;
real Gtottorq;
//<\INTERNAL>
//<CONSTANT>
// real Xplanet(1);
// real Yplanet(1);
// real Zplanet(1);
// real VXplanet(1);
// real VYplanet(1);
// real VZplanet(1);
// real MplanetVirtual(1);
// real Syk(Nz+2*NGHZ);
// real InvVj(Ny+2*NGHY);
// real xmin(Nx+2*NGHX+1);
// real ymin(Ny+2*NGHY+1);
// real zmin(Nz+2*NGHZ+1);
//<\CONSTANT>
//<MAIN_LOOP>
i = j = k = 0;
tottorq = 0;
#ifdef Z
for (k=0; k<size_z; k++) {
#endif
#ifdef Y
for (j=0; j<size_y; j++) {
#endif
#ifdef X
for (i=0; i<size_x; i++ ) {
#endif
//<#>
ll = l;
cellmass = Vol(j,k)*dens[ll];
#ifdef CARTESIAN
dx = xmed(i)-Xplanet;
dy = ymed(j)-Yplanet;
#ifdef Z
dz = zmed(k)-Zplanet;
#endif
#endif
#ifdef CYLINDRICAL
dx = ymed(j)*cos(xmed(i))-Xplanet;
dy = ymed(j)*sin(xmed(i))-Yplanet;
#ifdef Z
dz = zmed(k)-Zplanet;
#endif
#endif
#ifdef SPHERICAL
dx = ymed(j)*cos(xmed(i))*sin(zmed(k))-Xplanet;
dy = ymed(j)*sin(xmed(i))*sin(zmed(k))-Yplanet;
#ifdef Z
dz = ymed(j)*cos(zmed(k))-Zplanet;
#endif
#endif
dist2 = dx*dx+dy*dy+dz*dz;
dist2 += rsm2;
distance = sqrt(dist2);
InvDist3 = 1.0/(dist2*distance);
InvDist3 *= G*cellmass;
fxi = dx*InvDist3;
fyi = dy*InvDist3;
tottorq += Xplanet*fyi-Yplanet*fxi;
//<\#>
#ifdef X
}
#endif
#ifdef Y
}
#endif
#ifdef Z
}
#endif
//<\MAIN_LOOP>
MPI_Reduce (tottorq, Gtottorq, 1,MPI_DOUBLE,MPI_SUM,0,MPI_COMM_WORLD);
return Gtottorq;
}
/**
* construct from file name
*
* @param fileName file name
*/
Image3D::Image3D ( std::string fileName )
{
vol = Vol ( fileName.c_str() );
}
/**
* construct from size given by 2 integers
*
* @param width width of the image
* @param height height of the image
* @param depth depth of the image
*/
Image3D::Image3D ( int width, int height, int depth )
{
vol = Vol ( width, height, depth, 0 );
}
