本文整理汇总了C++中Vectors::empty方法的典型用法代码示例。如果您正苦于以下问题:C++ Vectors::empty方法的具体用法?C++ Vectors::empty怎么用?C++ Vectors::empty使用的例子?那么恭喜您, 这里精选的方法代码示例或许可以为您提供帮助。您也可以进一步了解该方法所在类Vectors
的用法示例。
在下文中一共展示了Vectors::empty方法的2个代码示例,这些例子默认根据受欢迎程度排序。您可以为喜欢或者感觉有用的代码点赞,您的评价将有助于系统推荐出更棒的C++代码示例。
示例1: solutionNorms
bool NonlinearDriver::solutionNorms (const TimeDomain& time,
double zero_tol, std::streamsize outPrec)
{
if (msgLevel < 0 || solution.empty()) return true;
const size_t nsd = model.getNoSpaceDim();
size_t iMax[nsd];
double dMax[nsd];
double normL2 = model.solutionNorms(solution.front(),dMax,iMax);
RealArray RF;
bool haveReac = model.getCurrentReactions(RF,solution.front());
Vectors gNorm;
if (calcEn)
{
model.setMode(SIM::RECOVERY);
model.setQuadratureRule(opt.nGauss[1]);
if (!model.solutionNorms(time,solution,gNorm))
gNorm.clear();
}
if (myPid > 0) return true;
std::streamsize stdPrec = outPrec > 0 ? IFEM::cout.precision(outPrec) : 0;
double old_tol = utl::zero_print_tol;
utl::zero_print_tol = zero_tol;
IFEM::cout <<" Primary solution summary: L2-norm : "
<< utl::trunc(normL2);
for (unsigned char d = 0; d < nsd; d++)
if (utl::trunc(dMax[d]) != 0.0)
IFEM::cout <<"\n Max "<< char('X'+d)
<<"-displacement : "<< dMax[d] <<" node "<< iMax[d];
if (haveReac)
{
IFEM::cout <<"\n Total reaction forces: Sum(R) =";
for (size_t i = 1; i < RF.size(); i++)
IFEM::cout <<" "<< utl::trunc(RF[i]);
if (utl::trunc(RF.front()) != 0.0)
IFEM::cout <<"\n displacement*reactions: (R,u) = "<< RF.front();
}
if (!gNorm.empty())
this->printNorms(gNorm.front(),IFEM::cout);
IFEM::cout << std::endl;
utl::zero_print_tol = old_tol;
if (stdPrec > 0) IFEM::cout.precision(stdPrec);
return true;
}
示例2: evalSol
bool Elasticity::evalSol (Vector& s, const Vectors& eV, const FiniteElement& fe,
const Vec3& X, bool toLocal, Vec3* pdir) const
{
if (eV.empty())
{
std::cerr <<" *** Elasticity::evalSol: No solutions vector."<< std::endl;
return false;
}
else if (!eV.front().empty() && eV.front().size() != fe.dNdX.rows()*nsd)
{
std::cerr <<" *** Elasticity::evalSol: Invalid displacement vector."
<<"\n size(eV) = "<< eV.front().size() <<" size(dNdX) = "
<< fe.dNdX.rows() <<","<< fe.dNdX.cols() << std::endl;
return false;
}
// Evaluate the deformation gradient, dUdX, and/or the strain tensor, eps
Matrix Bmat;
Tensor dUdX(nDF);
SymmTensor eps(nsd,axiSymmetry);
if (!this->kinematics(eV.front(),fe.N,fe.dNdX,X.x,Bmat,dUdX,eps))
return false;
// Add strains due to temperature expansion, if any
double epsT = this->getThermalStrain(eV.back(),fe.N,X);
if (epsT != 0.0) eps -= epsT;
// Calculate the stress tensor through the constitutive relation
Matrix Cmat;
SymmTensor sigma(nsd, axiSymmetry || material->isPlaneStrain()); double U;
if (!material->evaluate(Cmat,sigma,U,fe,X,dUdX,eps))
return false;
else if (epsT != 0.0 && nsd == 2 && material->isPlaneStrain())
sigma(3,3) -= material->getStiffness(X)*epsT;
Vec3 p;
bool havePval = false;
if (toLocal && wantPrincipalStress)
{
// Calculate principal stresses and associated direction vectors
if (sigma.size() == 4)
{
SymmTensor tmp(2); tmp = sigma; // discard the sigma_zz component
havePval = pdir ? tmp.principal(p,pdir,2) : tmp.principal(p);
}
else
havePval = pdir ? sigma.principal(p,pdir,2) : sigma.principal(p);
// Congruence transformation to local coordinate system at current point
if (locSys) sigma.transform(locSys->getTmat(X));
}
s = sigma;
if (toLocal)
s.push_back(sigma.vonMises());
if (havePval)
{
s.push_back(p.x);
s.push_back(p.y);
if (sigma.dim() == 3)
s.push_back(p.z);
}
return true;
}