Aerodynamics.hpp File Reference

#include <vulcan/core/VulcanTypes.hpp>
#include <janus/math/Linalg.hpp>
#include <janus/math/Logic.hpp>
#include <janus/math/Trig.hpp>

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Classes
struct	vulcan::aero::AeroState< Scalar >
	Complete aerodynamic state at a flight condition. More...

Namespaces
namespace	vulcan
namespace	vulcan::aero

Functions
template<typename Scalar>
Scalar	vulcan::aero::dynamic_pressure (const Scalar &density, const Scalar &velocity)
	Dynamic pressure.
template<typename Scalar>
Scalar	vulcan::aero::mach_number (const Scalar &velocity, const Scalar &speed_of_sound)
	Mach number.
template<typename Scalar>
Scalar	vulcan::aero::reynolds_number (const Scalar &density, const Scalar &velocity, const Scalar &length, const Scalar &viscosity)
	Reynolds number.
template<typename Scalar>
Scalar	vulcan::aero::airspeed (const Vec3< Scalar > &velocity_ground, const Vec3< Scalar > &velocity_wind)
	Compute airspeed from ground velocity and wind.
template<typename Scalar>
Scalar	vulcan::aero::airspeed (const Vec3< Scalar > &velocity)
	Compute airspeed magnitude from velocity vector.
template<typename Scalar>
Vec2< Scalar >	vulcan::aero::aero_angles (const Vec3< Scalar > &velocity_body)
	Compute aerodynamic angles from velocity in body frame.
template<typename Scalar>
AeroState< Scalar >	vulcan::aero::aero_state (const Scalar &density, const Scalar &speed_of_sound, const Scalar &viscosity, const Vec3< Scalar > &velocity_body, const Scalar &char_length)
	Compute complete aerodynamic state.