The Rankine–Hugoniot conditions, also referred to as Rankine–Hugoniot jump conditions or Rankine–Hugoniot relations, describe the relationship between the states on both sides of a shock wave in a one-dimensional flow in fluids or a one-dimensional deformation in solids. They are named in recognition of the work carried out by Scottish engineer and physicist William John Macquorn Rankine and French engineer Pierre Henri Hugoniot. See also Salas (2006) for some historical background.
In a coordinate system that is moving with the shock, the Rankine–Hugoniot conditions can be expressed as:
where us is the shock wave speed, ρ1 and ρ2 are the mass density of the fluid behind and inside the shock, u2 is the particle velocity of the fluid inside the shock, p1 and p2 are the pressures in the two regions, and E1 and E2 are the internal energies per unit mass in the two regions. A schematic of the quantities used in the above equations is shown in the adjacent figure. These equations can be derived in a straightforward manner from equations (12), (13) and (14) below. Using the Rankine-Hugoniot equations for the conservation of mass and momentum to eliminate us and u2, the equation for the conservation of energy can be expressed in the more popular form:
where v1 and v2 are the uncompressed and compressed specific volumes per unit mass, respectively.
Basics: Euler equations in one dimension
Consider gas in a one-dimensional container (e.g., a long thin tube). Assume that the fluid is inviscid (i.e., it shows no viscosity effects as for example friction with the tube walls). Furthermore, assume that there is no heat transfer by conduction or radiation and that gravitational acceleration can be neglected. Such a system can be described by the following system of conservation laws, known as the 1D Euler equations
- fluid mass density, [kg/m3]
- fluid velocity, [m/s]
- specific internal energy of the fluid, [J/kg]
- fluid pressure, [Pa]
- time, [s]
- distance, [m], and
- specific total energy of the fluid, [J/kg].
Assume further that the gas is calorically ideal and that therefore a polytropic equation-of-state of the simple form
is valid, where is the constant ratio of specific heats . This quantity also appears as the polytropic exponent of the polytropic process described by
Note: For a calorically ideal gas is a constant and for a thermally ideal gas is a function of temperature. In the latter case, the dependence of pressure on mass density and internal energy might differ from that given by equation (4).
The jump condition
Before proceeding further it is necessary to introduce the concept of a jump condition – a condition that holds at a discontinuity or abrupt change.
Consider a 1D situation where there is a jump in the scalar conserved physical quantity , which is governed by the hyperbolic conservation law
Let the solution exhibit a jump (or shock) at and integrate over the partial domain, , where and ,
The subscripts 1 and 2 indicate conditions just upstream and just downstream of the jump respectively. Note, to arrive at equation (8) we have used the fact that and .
Now, let and , when we have and , and in the limit
where we have defined (the system characteristic or shock speed), which by simple division is given by
Equation (9) represents the jump condition for conservation equation (6). A shock situation arises in a system where its characteristics intersect, and under these conditions a requirement for a unique single-valued solution is that the solution should satisfy the admissibility condition or entropy condition. For physically real applications this means that the solution should satisfy the Lax entropy condition
where and represent characteristic speeds at upstream and downstream conditions respectively.
Euler equations shock condition
In the case of the hyperbolic conservation equation (6), we have seen that the shock speed can be obtained by simple division. However, for the 1D Euler equations ( 1), ( 2) and ( 3), we have the vector state variable and the jump conditions become
Equations (12), (13) and (14) are known as the Rankine–Hugoniot conditions for the Euler equations and are derived by enforcing the conservation laws in integral form over a control volume that includes the shock. For this situation cannot be obtained by simple division. However, it can be shown by transforming the problem to a moving co-ordinate system (setting , , to remove ) and some algebraic manipulation (involving the elimination of from the transformed equation (13) using the transformed equation (12)), that the shock speed is given by
where is the speed of sound in the fluid at upstream conditions.
For a stationary shock , and for the 1D Euler equations we have
In view of equation (16) we can simplify equation (18) to
which is a statement of Bernoulli's principle, under conditions where gravitational effects can be neglected.
Substituting and from equations (16) and (17) into equation (19) yields the following relationship:
where represents specific enthalpy of the fluid. Eliminating internal energy in equation (19) by use of the equation-of-state, equation ( 4), yields
From physical considerations it is clear that both the upstream and downstream pressures must be positive, and this imposes an upper limit on the density ratio in equations (21) and (22) such that . As the strength of the shock increases, there is a corresponding increase in downstream gas temperature, but the density ratio approaches a finite limit: 4 for an ideal monatomic gas and 6 for an ideal diatomic gas . Note: air is comprised predominately of diatomic molecules and therefore at standard conditions .
Shock Hugoniot and Rayleigh line
For shocks in solids, a closed form expression such as equation (15) cannot be derived from first principles. Instead, experimental observations  indicate that a linear relation can be used instead (called the shock Hugoniot in the us-up plane) that has the form
where c0 is the bulk speed of sound in the material (in uniaxial compression), s is a parameter (the slope of the shock Hugoniot) obtained from fits to experimental data, and up=u2 is the particle velocity inside the compressed region behind the shock front.
The above relation, when combined with the Hugoniot equations for the conservation of mass and momentum, can be used to determine the shock Hugoniot in the p-v plane, where v is the specific volume (per unit mass):
Alternative equations of state, such as the Mie–Gruneisen equation of state may also be used instead of the above equation.
The shock Hugoniot describes the locus of all possible thermodynamic states a material can exist in behind a shock, projected onto a two dimensional state-state plane. It is therefore a set of equilibrium states and does not specifically represent the path through which a material undergoes transformation.
Weak shocks are isentropic and that the isentrope represents the path through which the material is loaded from the initial to final states by a compression wave with converging characteristics. In the case of weak shocks, the Hugoniot will therefore fall directly on the isentrope and can be used directly as the equivalent path. In the case of a strong shock we can no longer make that simplification directly. However, for engineering calculations, it is deemed that the isentrope is close enough to the Hugoniot that the same assumption can be made.
If the Hugoniot is approximately the loading path between states for an "equivalent" compression wave, then the jump conditions for the shock loading path can be determined by drawing a straight line between the initial and final states. This line is called the Rayleigh line and has the following equation:
Hugoniot elastic limit
Most solid materials undergo plastic deformations when subjected to strong shocks. The point on the shock Hugoniot at which a material transitions from a purely elastic state to an elastic-plastic state is called the Hugoniot elastic limit (HEL) and the pressure at which this transition takes place is denoted pHEL. Values of pHEL can range from 0.2 GPa to 20 GPa. Above the HEL, the material loses much of its shear strength and starts behaving like a fluid.
- Calculate normal shock wave parameters for mixtures of imperfect gases. Gas Dynamics Toolbox
- Shock polar
- Mie–Gruneisen equation of state
- Engineering Acoustics Wikibook
- Rankine, W. J. M. (1870). "On the thermodynamic theory of waves of finite longitudinal disturbances". Philosophical Transactions of the Royal Society of London 160: 277–288. doi:10.1098/rstl.1870.0015.
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