star_rot_isco.C

/*
 * Method of class Star_rot to compute the location of the ISCO
 *
 * (see file star_rot.h for documentation).
 *
 */
 
/*
 *   Copyright (c) 2010 Eric Gourgoulhon
 *   Copyright (c) 2000-2001 J. Leszek Zdunik
 *
 *   This file is part of LORENE.
 *
 *   LORENE is free software; you can redistribute it and/or modify
 *   it under the terms of the GNU General Public License as published by
 *   the Free Software Foundation; either version 2 of the License, or
 *   (at your option) any later version.
 *
 *   LORENE is distributed in the hope that it will be useful,
 *   but WITHOUT ANY WARRANTY; without even the implied warranty of
 *   MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE.  See the
 *   GNU General Public License for more details.
 *
 *   You should have received a copy of the GNU General Public License
 *   along with LORENE; if not, write to the Free Software
 *   Foundation, Inc., 59 Temple Place, Suite 330, Boston, MA  02111-1307  USA
 *
 */
 
 
 
 
/*
 * $Id: star_rot_isco.C,v 1.6 2016/12/05 16:18:15 j_novak Exp $
 * $Log: star_rot_isco.C,v $
 * Revision 1.6  2016/12/05 16:18:15  j_novak
 * Suppression of some global variables (file names, loch, ...) to prevent redefinitions
 *
 * Revision 1.5  2014/10/13 08:53:39  j_novak
 * Lorene classes and functions now belong to the namespace Lorene.
 *
 * Revision 1.4  2014/10/06 15:13:17  j_novak
 * Modified #include directives to use c++ syntax.
 *
 * Revision 1.3  2011/01/07 18:20:21  m_bejger
 * Correcting for the case of stiff EOS, in which ISCO may be farther than the first domain outside the star - now searching all non-compactified domains
 *
 * Revision 1.2  2010/01/25 22:33:04  e_gourgoulhon
 * First implementation.
 *
 * Revision 1.1  2010/01/25 18:15:52  e_gourgoulhon
 * First version.
 *
 *
 * $Header: /cvsroot/Lorene/C++/Source/Star/star_rot_isco.C,v 1.6 2016/12/05 16:18:15 j_novak Exp $
 *
 */
 
// Headers C
#include <cmath>
 
// Headers Lorene
#include "star_rot.h"
#include "param.h"
#include "utilitaires.h"
 
namespace Lorene {
double funct_star_rot_isco(double, const Param& ) ; 
 
//=============================================================================
//      r_isco()
//=============================================================================
 
double Star_rot::r_isco(ostream* ost) const {
 
    if (p_r_isco == 0x0) {    // a new computation is required
 
    // First and second derivatives of metric functions
    // ------------------------------------------------
 
    int nzm1 = mp.get_mg()->get_nzone() - 1 ;
    Scalar dnphi = nphi.dsdr() ;
    dnphi.annule_domain(nzm1) ;
    Scalar ddnphi = dnphi.dsdr() ;      // d^2/dr^2 N^phi
 
    Scalar tmp = nn.dsdr() ;
    tmp.annule_domain(nzm1) ;
    Scalar ddnnn = tmp.dsdr() ;         // d^2/dr^2 N
 
    tmp = bbb.dsdr() ;
    tmp.annule_domain(nzm1) ;
    Scalar ddbbb = tmp.dsdr() ;         // d^2/dr^2 B
 
    // Constructing the velocity of a particle corotating with the star
    // ----------------------------------------------------------------
 
    Scalar bdlog = bbb.dsdr() / bbb ;
    Scalar ndlog = nn.dsdr() / nn ;
    Scalar bsn = bbb / nn ;
 
    Scalar r(mp) ;
    r = mp.r ;
 
    Scalar r2= r*r ;
 
    bdlog.annule_domain(nzm1) ;
    ndlog.annule_domain(nzm1) ;
    bsn.annule_domain(nzm1) ;
    r2.annule_domain(nzm1) ;
 
    // ucor_plus - the velocity of corotating particle on the circular orbit
    Scalar ucor_plus = (r2 * bsn * dnphi +
        sqrt ( r2 * r2 * bsn *bsn * dnphi * dnphi +
        4 * r2 * bdlog * ndlog + 4 * r * ndlog) ) /
        2 / (1 + r * bdlog ) ;
 
    Scalar factor_u2 = r2 * (2 * ddbbb / bbb - 2 * bdlog * bdlog +
                          4 * bdlog * ndlog ) +
       2 * r2 * r2 * bsn * bsn * dnphi * dnphi +
       4 * r * ( ndlog - bdlog ) - 6 ;
 
    Scalar factor_u1 = 2 * r * r2 * bsn * ( 2 * ( ndlog - bdlog ) *
                    dnphi - ddnphi ) ;
 
    Scalar factor_u0 = - r2 * ( 2 * ddnnn / nn - 2 * ndlog * ndlog +
                     4 * bdlog * ndlog ) ;
 
    // Scalar field the zero of which will give the marginally stable orbit
    Scalar orbit = factor_u2 * ucor_plus * ucor_plus +
                factor_u1 * ucor_plus + factor_u0 ;
    orbit.std_spectral_base() ;
    
    // Search for the zero
    // -------------------
 
    double r_ms, theta_ms, phi_ms, xi_ms, 
           xi_min = -1, xi_max = 1; 
    int l_ms = nzet, l ;
    bool find_status = false ; 
 
    const Valeur& vorbit = orbit.get_spectral_va() ;
        
    for(l = nzet; l <= nzm1; l++) { 
 
    // Preliminary location of the zero
    // of the orbit function with an error = 0.01
    theta_ms = M_PI / 2. ; // pi/2
    phi_ms = 0. ;
 
    xi_min = -1. ;
    xi_max = 1. ;
 
    double resloc_old ;
    double xi_f = xi_min;
    
    double resloc = vorbit.val_point(l, xi_min, theta_ms, phi_ms) ;
    
    for (int iloc=0; iloc<200; iloc++) {
        xi_f = xi_f + 0.01 ;
        resloc_old = resloc ;
        resloc = vorbit.val_point(l, xi_f, theta_ms, phi_ms) ;
        if ( resloc * resloc_old < double(0) ) {
            xi_min = xi_f - 0.01 ;
            xi_max = xi_f ;
            l_ms = l ; 
            find_status = true ;  
            break ;
        } 
        
      }
    
    } 
    
    Param par_ms ;
    par_ms.add_int(l_ms) ;
    par_ms.add_scalar(orbit) ;
    
    if(find_status) { 
                            
        double precis_ms = 1.e-12 ;    // precision in the determination 
                                       // of xi_ms
        int nitermax_ms = 100 ;        // max number of iterations
 
        int niter ;
        xi_ms = zerosec(funct_star_rot_isco, par_ms, xi_min, xi_max,
                        precis_ms, nitermax_ms, niter) ;                        
        if (ost != 0x0) {
            * ost <<
            "    number of iterations used in zerosec to locate the ISCO : "
             << niter << endl ;
            *ost << "    zero found at xi = " << xi_ms << endl ;
        }
 
        r_ms = mp.val_r(l_ms, xi_ms, theta_ms, phi_ms) ;
    
    } else { 
        
        // assuming the ISCO is under the surface of a star 
        r_ms = ray_eq() ; 
        xi_ms = -1 ; 
        l_ms = nzet ; 
        
    } 
    
    p_r_isco = new double (
        (bbb.get_spectral_va()).val_point(l_ms, xi_ms, theta_ms, phi_ms) * r_ms
                          ) ;
 
    // Determination of the frequency at the marginally stable orbit
    // -------------------------------------------------------------                
 
    ucor_plus.std_spectral_base() ;
    double ucor_msplus = (ucor_plus.get_spectral_va()).val_point(l_ms, xi_ms, theta_ms,
                                                  phi_ms) ;
    double nobrs = (bsn.get_spectral_va()).val_point(l_ms, xi_ms, theta_ms, phi_ms) ;
    double nphirs = (nphi.get_spectral_va()).val_point(l_ms, xi_ms, theta_ms, phi_ms) ;
    
    p_f_isco = new double ( ( ucor_msplus / nobrs / r_ms + nphirs ) /
                                (double(2) * M_PI) ) ;
 
    // Specific angular momentum on ms orbit
    // -------------------------------------                
    p_lspec_isco=new double (ucor_msplus/sqrt(1.-ucor_msplus*ucor_msplus)*
    ((bbb.get_spectral_va()).val_point(l_ms, xi_ms, theta_ms, phi_ms)) * r_ms );
 
    // Specific energy on ms orbit
    // ---------------------------          
    p_espec_isco=new double (( 1./nobrs / r_ms / ucor_msplus  + nphirs) *
    (ucor_msplus/sqrt(1.-ucor_msplus*ucor_msplus)*
    ((bbb.get_spectral_va()).val_point(l_ms, xi_ms, theta_ms, phi_ms)) * r_ms ));
 
        // Determination of the Keplerian frequency at the equator
    // -------------------------------------------------------------
 
 
    double ucor_eqplus = (ucor_plus.get_spectral_va()).val_point(l_ms, -1, theta_ms,phi_ms)
      ;
    double nobeq = (bsn.get_spectral_va()).val_point(l_ms, -1, theta_ms, phi_ms) ;
    double nphieq = (nphi.get_spectral_va()).val_point(l_ms, -1, theta_ms, phi_ms) ;
 
    p_f_eq = new double ( ( ucor_eqplus / nobeq / ray_eq() + nphieq ) /
                  (double(2) * M_PI) ) ;
 
    
 
    }  // End of computation
 
    return *p_r_isco ;
 
}
 
 
 
//=============================================================================
//      f_isco()
//=============================================================================
 
double Star_rot::f_isco() const {
 
    if (p_f_isco == 0x0) {    // a new computation is required
 
        r_isco() ;      // f_isco is computed in the method r_isco()
 
        assert(p_f_isco != 0x0) ;
    }
 
    return *p_f_isco ;
 
}
 
//=============================================================================
//      lspec_isco()
//=============================================================================
 
double Star_rot::lspec_isco() const {
 
    if (p_lspec_isco == 0x0) {    // a new computation is required
 
        r_isco() ;  // lspec_isco is computed in the method r_isco()
 
        assert(p_lspec_isco != 0x0) ;
    }
 
    return *p_lspec_isco ;
 
}
 
//=============================================================================
//      espec_isco()
//=============================================================================
 
double Star_rot::espec_isco() const {
 
    if (p_espec_isco == 0x0) {    // a new computation is required
 
        r_isco() ;  // espec_isco is computed in the method r_isco()
 
        assert(p_espec_isco != 0x0) ;
    }
 
    return *p_espec_isco ;
 
}
 
 
//=============================================================================
//              f_eq()
//=============================================================================
 
double Star_rot::f_eq() const {
  
  if (p_f_eq == 0x0) {    // a new computation is required
 
    r_isco() ;              // f_eq is computed in the method r_isco()
 
    assert(p_f_eq != 0x0) ;
  }
 
  return *p_f_eq ;
 
}
 
 
//=============================================================================
//  Function used to locate the MS orbit
//=============================================================================
 
 
double funct_star_rot_isco(double xi, const Param& par){
 
    // Retrieval of the information:
    int l_ms = par.get_int() ;
    const Scalar& orbit = par.get_scalar() ;
    const Valeur& vorbit = orbit.get_spectral_va() ;
 
    // Value et the desired point
    double theta = M_PI / 2. ;
    double phi = 0 ;
    return vorbit.val_point(l_ms, xi, theta, phi) ;
 
}
 
 
 
 
 
 
}