Chaplygin's equation

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In gas dynamics, Chaplygin's equation, named after Sergei Alekseevich Chaplygin (1902), is a partial differential equation useful in the study of transonic flow.[1] It is

2Φθ2+v21v2/c22Φv2+vΦv=0.

Here, c=c(v) is the speed of sound, determined by the equation of state of the fluid and conservation of energy. For polytropic gases, we have c2/(γ1)=h0v2/2, where γ is the specific heat ratio and h0 is the stagnation enthalpy, in which case the Chaplygin's equation reduces to

2Φθ2+v22h0v22h0(γ+1)v2/(γ1)2Φv2+vΦv=0.

The Bernoulli equation (see the derivation below) states that maximum velocity occurs when specific enthalpy is at the smallest value possible; one can take the specific enthalpy to be zero corresponding to absolute zero temperature as the reference value, in which case 2h0 is the maximum attainable velocity. The particular integrals of above equation can be expressed in terms of hypergeometric functions.[2][3]

Derivation

For two-dimensional potential flow, the continuity equation and the Euler equations (in fact, the compressible Bernoulli's equation due to irrotationality) in Cartesian coordinates (x,y) involving the variables fluid velocity (vx,vy), specific enthalpy h and density ρ are

x(ρvx)+y(ρvy)=0,h+12v2=ho.

with the equation of state ρ=ρ(s,h) acting as third equation. Here ho is the stagnation enthalpy, v2=vx2+vy2 is the magnitude of the velocity vector and s is the entropy. For isentropic flow, density can be expressed as a function only of enthalpy ρ=ρ(h), which in turn using Bernoulli's equation can be written as ρ=ρ(v).

Since the flow is irrotational, a velocity potential ϕ exists and its differential is simply dϕ=vxdx+vydy. Instead of treating vx=vx(x,y) and vy=vy(x,y) as dependent variables, we use a coordinate transform such that x=x(vx,vy) and y=y(vx,vy) become new dependent variables. Similarly the velocity potential is replaced by a new function (Legendre transformation)[4]

Φ=xvx+yvyϕ

such then its differential is dΦ=xdvx+ydvy, therefore

x=Φvx,y=Φvy.

Introducing another coordinate transformation for the independent variables from (vx,vy) to (v,θ) according to the relation vx=vcosθ and vy=vsinθ, where v is the magnitude of the velocity vector and θ is the angle that the velocity vector makes with the vx-axis, the dependent variables become

x=cosθΦvsinθvΦθ,y=sinθΦv+cosθvΦθ,ϕ=Φ+vΦv.

The continuity equation in the new coordinates become

d(ρv)dv(Φv+1v2Φθ2)+ρv2Φv2=0.

For isentropic flow, dh=ρ1c2dρ, where c is the speed of sound. Using the Bernoulli's equation we find

d(ρv)dv=ρ(1v2c2)

where c=c(v). Hence, we have

2Φθ2+v21v2c22Φv2+vΦv=0.

See also

References

  1. Chaplygin, S. A. (1902). On gas streams. Complete collection of works.(Russian) Izd. Akad. Nauk SSSR, 2.
  2. Sedov, L. I., (1965). Two-dimensional problems in hydrodynamics and aerodynamics. Chapter X
  3. Von Mises, R., Geiringer, H., & Ludford, G. S. S. (2004). Mathematical theory of compressible fluid flow. Courier Corporation.
  4. Landau, L. D.; Lifshitz, E. M. (1982). Fluid Mechanics (2 ed.). Pergamon Press. p. 432.