aerodynamics.hpp File Reference

#include <algorithm>
#include <array>
#include <cassert>
#include <cmath>
#include <ranges>
#include <span>
#include <vector>
#include "aerodynamics_input.hpp"
#include "interfaces/host_state.hpp"
#include "math/interpolation.hpp"
#include "math/quaternion_operations.hpp"
#include "math/vector_operations.hpp"
#include "model/node.hpp"

Go to the source code of this file.

Classes
class	kynema::interfaces::components::AerodynamicBody
class	kynema::interfaces::components::Aerodynamics

Namespaces
namespace	kynema
namespace	kynema::interfaces
namespace	kynema::interfaces::components

Functions
double	kynema::interfaces::components::CalculateAngleOfAttack (std::span< const double, 3 > v_rel)
std::array< double, 6 >	kynema::interfaces::components::CalculateAerodynamicLoad (std::span< double, 3 > ref_axis_moment, std::span< const double, 3 > v_inflow, std::span< const double, 3 > v_motion, std::span< const double > aoa_polar, std::span< const double > cl_polar, std::span< const double > cd_polar, std::span< const double > cm_polar, double chord, double delta_s, double fluid_density, std::span< const double, 3 > con_force, std::span< const double, 4 > qqr)
std::array< double, 3 >	kynema::interfaces::components::CalculateConMotionVector (double ac_to_ref_axis_horizontal, double chord_to_ref_axis_vertical)
std::vector< double >	kynema::interfaces::components::CalculateJacobianXi (std::span< const double > aero_node_xi)
std::vector< double >	kynema::interfaces::components::CalculateAeroNodeWidths (std::span< const double > jacobian_xi, std::span< const double > jacobian_integration_matrix, std::span< const double > node_x)