qtrocket/sim/Aero.h
Travis Hunter e6bf1fea9b
Some checks failed
CMake on multiple platforms / build (Release, cl, cl, windows-latest) (push) Has been cancelled
CMake on multiple platforms / build (Release, gcc-13, g++-13, ubuntu-latest) (push) Has been cancelled
Revert "Merge pull request #20 from cthunter01/propagator"
This reverts commit 6280d9fb0184275843a8f4406c7293e41e65a639, reversing
changes made to 3c9c8b8c6a2b2e7430ff09efdc2cc0c1996b16ca.
2025-04-16 18:23:28 -06:00

41 lines
694 B
C++

#ifndef SIM_AERO_H
#define SIM_AERO_H
/// \cond
// C headers
// C++ headers
// 3rd party headers
/// \endcond
// qtrocket headers
#include "utils/math/MathTypes.h"
namespace sim
{
class Aero
{
public:
private:
Vector3 cp; /// center of pressure
double Cx; /// longitudinal coefficient
double Cy; /// These are probably the same for axial symmetric
double Cz; /// rockets. The coeffients in the y and z body directions
double Cl; // roll moment coefficient
double Cm; // pitch moment coefficient
double Cn; // yaw moment coefficient
double baseCd; // coefficient of drag due to base drag
double Cd; // total coeffient of drag
};
}
#endif // SIM_AERO_H