/**
* \file aero_coeff_control.h
* \author basile.graf@epfl.ch
* 
* This file contains stuff related to Lift and Drag computation... 
*/


#ifndef AERO_COEFF_CONTR_H_DEF 
#define AERO_COEFF_CONTR_H_DEF  

/// Aoero/nautical coefficients computing
/**
* Computes lift and drag coefficients for all surfaces/bodies. \n
* Polynomial forms are used, polar tables are still to be implemented!!
* \param *d : pointer to the datas data-structure
*/
 void aero_coeff_control(datas *d);
 
#endif 