PHengLEI-NCCR/API/Physics/include/AerodynamicsBasicRelations.h

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//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
// PPPPP H H EEEEE N N GGGGG L EEEEE III +
// P P H H E NN N G L E I +
// PPPPP HHHHH EEEEE N N N G GG L EEEEE I +
// P H H E N N N G G L E I +
// P H H EEEEE N N GGGGG LLLLL EEEEE III +
//------------------------------------------------------------------------+
// Platform for Hybrid Engineering Simulation of Flows +
// China Aerodynamics Research and Development Center +
// (C) Copyright, Since 2010 +
//+++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
//! @file Aerodynamics_BasicRelations.h
//! @brief Define some basic aerodynamic relations, e.g isentropic relations, shock relations.
//! @author Zhang Jian, He Xin.
#pragma once
#include "Precision.h"
namespace PHSPACE
{
//! isentropic relationships
struct IsentropicRelations{
//! T0/T
static RDouble T0OverT(RDouble gama, RDouble mach);
//! P0/P
static RDouble P0OverP(RDouble gama, RDouble mach);
//! Rho0/Rho
static RDouble Rho0OverRho(RDouble gama, RDouble mach);
};
struct ShockRelations{
//! Behind/Before shock temperature relation
//! @param gama gama
//! @param m1 mach before the shock
static RDouble T2OverT1(RDouble gama, RDouble m1);
//! Behind/Before shock pressure relation
//! @param gama gama
//! @param m1 mach before the shock
static RDouble P2OverP1(RDouble gama, RDouble m1);
//! Behind/Before shock density relation
//! @param gama gama
//! @param m1 mach before the shock
static RDouble Rho2OverRho1(RDouble gama, RDouble m1);
//! Compute mach behind the shock by mach before the shock
//! @param gama gama
//! @param m1 mach before the shock
static RDouble MachBehindShock(RDouble gama, RDouble m1);
};
}