20 #ifndef __mast__time_domain_flutter_solver_h__ 21 #define __mast__time_domain_flutter_solver_h__ 35 class TimeDomainFlutterSolution;
77 unsigned int n_V_divs,
78 std::vector<libMesh::NumericVector<Real>*>& basis);
104 virtual std::pair<bool, MAST::FlutterRootBase*>
106 const unsigned int n_bisection_iters);
115 virtual std::pair<bool, MAST::FlutterRootBase*>
117 const unsigned int n_bisection_iters);
125 virtual std::pair<bool, MAST::FlutterRootBase*>
127 const unsigned int n_iters);
144 libMesh::NumericVector<Real>* dXdp =
nullptr,
145 libMesh::NumericVector<Real>* dXdV =
nullptr);
177 virtual std::unique_ptr<MAST::TimeDomainFlutterSolution>
186 virtual std::pair<bool, MAST::FlutterSolutionBase*>
189 const unsigned int root_num,
191 const unsigned int max_iters);
209 const libMesh::NumericVector<Real>& dXdp,
256 #endif // __mast__time_domain_flutter_solver_h__
TimeDomainFlutterSolver()
defalut constructor
virtual std::pair< bool, MAST::FlutterRootBase * > analyze_and_find_critical_root_without_tracking(const Real g_tol, const unsigned int n_iters)
This root starts with the lower velocity and increments the speed till a single unstable root is iden...
virtual void _identify_crossover_points()
identifies all cross-over and divergence points from analyzed roots
MAST::Parameter * _velocity_param
Parameter that define the velocity.
virtual void clear()
clears the solution and other data from this solver
virtual void calculate_sensitivity(MAST::FlutterRootBase &root, const MAST::FunctionBase &f, libMesh::NumericVector< Real > *dXdp=nullptr, libMesh::NumericVector< Real > *dXdV=nullptr)
Calculate the sensitivity of the flutter root with respect to the f parameter.
virtual void print_crossover_points()
Prints the crossover points output.
void initialize(MAST::Parameter &velocity_param, Real V_lower, Real V_upper, unsigned int n_V_divs, std::vector< libMesh::NumericVector< Real > * > &basis)
initializes the data structres for a flutter solution.
This is a scalar function whose value can be changed and one that can be used as a design variable in...
virtual std::unique_ptr< MAST::TimeDomainFlutterSolution > _analyze(const Real v_ref, const MAST::FlutterSolutionBase *prev_sol=nullptr)
performs an eigensolution at the specified reference value, and sort the roots based on the provided ...
std::multimap< Real, MAST::FlutterRootCrossoverBase * > _flutter_crossovers
the map of flutter crossover points versus average velocity of the two bounding roots ...
void _initialize_matrices(Real U_inf, RealMatrixX &A, RealMatrixX &B)
Assembles the reduced order system structural and aerodynmaic matrices for specified flight velocity ...
virtual std::pair< bool, MAST::FlutterSolutionBase * > _bisection_search(const std::pair< MAST::FlutterSolutionBase *, MAST::FlutterSolutionBase * > &ref_sol_range, const unsigned int root_num, const Real g_tol, const unsigned int max_iters)
bisection method search
virtual void print_sorted_roots()
Prints the sorted roots to the output.
Matrix< Real, Dynamic, Dynamic > RealMatrixX
virtual ~TimeDomainFlutterSolver()
virtual unsigned int n_roots_found() const
finds the number of critical points already identified in the procedure.
std::pair< Real, Real > _V_range
range of reference values within which to find flutter roots
virtual void scan_for_roots()
Scans for flutter roots in the analyzed points, and identified the divergence (if k_red = 0...
virtual std::pair< bool, MAST::FlutterRootBase * > find_critical_root(const Real g_tol, const unsigned int n_bisection_iters)
This method checks if the flutter root corresponding to the lowest velocity crossover has been calcul...
This implements a solver for a single parameter instability problem, for example a flutter solver whe...
unsigned int _n_V_divs
number of division in the reference value range for initial scanning
virtual void clear_solutions()
clears the solutions stored from a previous analysis.
std::map< Real, MAST::FlutterSolutionBase * > _flutter_solutions
map of velocity sorted flutter solutions
void _initialize_matrix_sensitivity_for_param(const MAST::FunctionBase &f, const libMesh::NumericVector< Real > &dXdp, Real U_inf, RealMatrixX &A, RealMatrixX &B)
Assembles the reduced order system structural and aerodynmaic matrices for specified flight velocity ...
virtual std::pair< bool, MAST::FlutterRootBase * > find_next_root(const Real g_tol, const unsigned int n_bisection_iters)
Looks through the list of flutter cross-over points and iteratively zooms in to find the cross-over p...
const MAST::FlutterRootBase & get_root(const unsigned int n) const
returns the n th root in terms of ascending velocity that is found by the solver