Airfoil2DRigid.h

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/*--------------------------------*- VM2D -*-----------------*---------------*\
| ##  ## ##   ##  ####  #####   |                            | Version 1.14   |
| ##  ## ### ### ##  ## ##  ##  |  VM2D: Vortex Method       | 2026/03/06     |
| ##  ## ## # ##    ##  ##  ##  |  for 2D Flow Simulation    *----------------*
|  ####  ##   ##   ##   ##  ##  |  Open Source Code                           |
|   ##   ##   ## ###### #####   |  https://www.github.com/vortexmethods/VM2D  |
|                                                                             |
| Copyright (C) 2017-2026 I. Marchevsky, K. Sokol, E. Ryatina, A. Kolganova   |
*-----------------------------------------------------------------------------*
| File name: Airfoil2DRect.h                                                  |
| Info: Source code of VM2D                                                   |
|                                                                             |
| This file is part of VM2D.                                                  |
| VM2D 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 3 of the License, or           |
| (at your option) any later version.                                         |
|                                                                             |
| VM2D 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 VM2D.  If not, see <http://www.gnu.org/licenses/>.               |
\*---------------------------------------------------------------------------*/
 
 
#ifndef AIRFOILRECT_H
#define AIRFOILRECT_H
 
#include "Airfoil2D.h"
 
namespace VM2D
{
 
    class World2D;
 
    class AirfoilRigid
        : public Airfoil
    {
    public:
 
        AirfoilRigid(const World2D& W_, const size_t numberInPassport_)
            :Airfoil(W_, numberInPassport_)
        { };
 
        AirfoilRigid(const Airfoil& afl) : Airfoil(afl) {};
 
        virtual ~AirfoilRigid() { };
        
        //void CalcNrmTauLen();
 
//      ///Вычисляет габаритный прямоугольник профиля
//      virtual void GetGabarits(double gap = 0.02) override;
//
//      //далее -- реализация виртуальных функций
//      virtual void ReadFromFile(const std::string& dir) override;
//      virtual void Rotate(double alpha) override;
//      virtual void Scale(const Point2D&) override;
//      virtual void Move(const Point2D& dr) override;
//      
//      virtual std::vector<double> getA(size_t p, size_t i, const Airfoil& airfoil, size_t j) const override;
//      virtual void calcIQ(size_t p, const Airfoil& otherAirfoil, std::pair<Eigen::MatrixXd, Eigen::MatrixXd>& matrPair) const override;
//
//      virtual bool IsPointInAirfoil(const Point2D& point) const override;
//
//      virtual void GetDiffVelocityI0I3ToSetOfPointsAndViscousStresses(const WakeDataBase& pointsDb, std::vector<double>& domainRadius, std::vector<double>& I0, std::vector<Point2D>& I3) override;
//#if defined(USE_CUDA)
//      virtual void GPUGetDiffVelocityI0I3ToSetOfPointsAndViscousStresses(const WakeDataBase& pointsDb, std::vector<double>& domainRadius, std::vector<double>& I0, std::vector<Point2D>& I3) override;
//#endif
//      virtual void GetDiffVelocityI0I3ToWakeAndViscousStresses(const WakeDataBase& pointsDb, std::vector<double>& domainRadius, std::vector<double>& I0, std::vector<Point2D>& I3) override;
//
//      virtual void GetInfluenceFromVorticesToPanel(size_t panel, const Vortex2D* ptr, ptrdiff_t count, std::vector<double>& panelRhs) const override;
//      virtual void GetInfluenceFromSourcesToPanel(size_t panel, const Vortex2D* ptr, ptrdiff_t count, std::vector<double>& panelRhs) const override;
//
//      virtual void GetInfluenceFromSourceSheetToVortex(size_t panel, const Vortex2D& vtx, Point2D& vel) const override;
//      virtual void GetInfluenceFromVortexSheetToVortex(size_t panel, const Vortex2D& vtx, Point2D& vel) const override;
//
//      virtual void GetInfluenceFromVInfToPanel(std::vector<double>& vInfRhs) const override;
    };
 
}//namespace VM2D
 
#endif