Riemann invariant

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Riemann invariants are mathematical transformations made on a system of conservation equations to make them more easily solvable. Riemann invariants are constant along the characteristic curves of the partial differential equations where they obtain the name invariant. They were first obtained by Bernhard Riemann in his work on plane waves in gas dynamics.[1]

Mathematical theory

Consider the set of conservation equations:

li(Aijujt+aijujx)+ljbj=0

where Aij and aij are the elements of the matrices 𝐀 and 𝐚 where li and bi are elements of vectors. It will be asked if it is possible to rewrite this equation to

mj(βujt+αujx)+ljbj=0

To do this curves will be introduced in the (x,t) plane defined by the vector field (α,β). The term in the brackets will be rewritten in terms of a total derivative where x,t are parametrized as x=X(η),t=T(η)

dujdη=Tujt+Xujx

comparing the last two equations we find

α=X(η),β=T(η)

which can be now written in characteristic form

mjdujdη+ljbj=0

where we must have the conditions

liAij=mjT
liaij=mjX

where mj can be eliminated to give the necessary condition

li(AijXaijT)=0

so for a nontrivial solution is the determinant

|AijXaijT|=0

For Riemann invariants we are concerned with the case when the matrix 𝐀 is an identity matrix to form

uit+aijujx=0

notice this is homogeneous due to the vector 𝐧 being zero. In characteristic form the system is

liduidt=0 with dxdt=λ

Where l is the left eigenvector of the matrix 𝐀 and λs is the characteristic speeds of the eigenvalues of the matrix 𝐀 which satisfy

|Aλδij|=0

To simplify these characteristic equations we can make the transformations such that drdt=liduidt

which form

μlidui=dr

An integrating factor μ can be multiplied in to help integrate this. So the system now has the characteristic form

drdt=0 on dxdt=λi

which is equivalent to the diagonal system[2]

rtk+λkrxk=0, k=1,...,N.

The solution of this system can be given by the generalized hodograph method.[3][4]

Example

Consider the one-dimensional Euler equations written in terms of density ρ and velocity u are

ρt+ρux+uρx=0
ut+uux+(c2/ρ)ρx=0

with c being the speed of sound is introduced on account of isentropic assumption. Write this system in matrix form

(ρu)t+(uρc2ρu)(ρu)x=(00)

where the matrix 𝐚 from the analysis above the eigenvalues and eigenvectors need to be found. The eigenvalues are found to satisfy

λ22uλ+u2c2=0

to give

λ=u±c

and the eigenvectors are found to be

(1cρ),(1cρ)

where the Riemann invariants are

r1=J+=u+cρdρ,
r2=J=ucρdρ,

(J+ and J are the widely used notations in gas dynamics). For perfect gas with constant specific heats, there is the relation c2=constγργ1, where γ is the specific heat ratio, to give the Riemann invariants[5][6]

J+=u+2γ1c,
J=u2γ1c,

to give the equations

J+t+(u+c)J+x=0
Jt+(uc)Jx=0

In other words,

dJ+=0,J+=constalongC+:dxdt=u+c,dJ=0,J=constalongC:dxdt=uc,

where C+ and C are the characteristic curves. This can be solved by the hodograph transformation. In the hodographic plane, if all the characteristics collapses into a single curve, then we obtain simple waves. If the matrix form of the system of pde's is in the form

Avt+Bvx=0

Then it may be possible to multiply across by the inverse matrix A1 so long as the matrix determinant of 𝐀 is not zero.

See also

References

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Template:Bernhard Riemann

  1. Template:Cite journal
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  5. Zelʹdovich, I. B., & Raĭzer, I. P. (1966). Physics of shock waves and high-temperature hydrodynamic phenomena (Vol. 1). Academic Press.
  6. Courant, R., & Friedrichs, K. O. 1948 Supersonic flow and shock waves. New York: Interscience.