Waves in blood vessels

The flow of blood in our bodies is basically fluid flow in a network of pipes. Unlike rigid pipes, the walls in the blood vessels are elastic and will increase their diameter when the pressure rises. The elastic forces will then push the wall back and accelerate the fluid. This interaction between the flow of blood and the deformation of the vessel wall results in waves traveling along our blood vessels.

A model for one-dimensional waves along blood vessels can be derived from averaging the fluid flow over the cross section of the blood vessels. Let x be a coordinate along the blood vessel and assume that all cross sections are circular, though with different radii R(x,t). The main quantities to compute is the cross section area A(x,t), the averaged pressure P(x,t), and the total volume flux Q(x,t). The area of this cross section is

A(x,t)=2πR(x,t)0rdr,

Let vx(x,t) be the velocity of blood averaged over the cross section at point x. The volume flux, being the total volume of blood passing a cross section per time unit, becomes

Q(x,t)=A(x,t)vx(x,t)

Mass balance and Newton’s second law lead to the PDEs

At+Qx=0,
Qt+γ+2γ+1x(Q2A)+AϱPx=2π(γ+2)μϱQA,

where γ is a parameter related to the velocity profile, ϱ is the density of blood, and μ is the dynamic viscosity of blood.

We have three unknowns A, Q, and P, and two equations (158) and (159). A third equation is needed to relate the flow to the deformations of the wall. A common form for this equation is

Pt+1CQx=0,

where C is the compliance of the wall, given by the constitutive relation

C=AP+At,

which require a relationship between A and P. One common model is to view the vessel wall, locally, as a thin elastic tube subject to an internal pressure. This gives the relation

P=P0+πhE(1ν2)A0(AA0),

where P0 and A0 are corresponding reference values when the wall is not deformed, h is the thickness of the wall, and E and ν are Young’s modulus and Poisson’s ratio of the elastic material in the wall. The derivative becomes

C=AP=2(1ν2)A0πhEA0+2((1ν2)A0πhE)2(PP0).

Another (nonlinear) deformation model of the wall, which has a better fit with experiments, is

P=P0exp(β(A/A01)),

where β is some parameter to be estimated. This law leads to

C=AP=A0βP.

Reduction to the standard wave equation. It is not uncommon to neglect the viscous term on the right-hand side of (159) and also the quadratic term with Q2 on the left-hand side. The reduced equations (159) and (160) form a first-order linear wave equation system:

CPt=Qx,
Qt=AϱPx.

These can be combined into standard 1D wave equation PDE by differentiating the first equation with respect t and the second with respect to x,

t(CPt)=x(AϱPx),

which can be approximated by

2Qt2=c22Qx2,c=AϱC,

where the A and C in the expression for c are taken as constant reference values.

Electromagnetic waves

Light and radio waves are governed by standard wave equations arising from Maxwell’s general equations. When there are no charges and no currents, as in a vacuum, Maxwell’s equations take the form

EE=0,BB=0,×EE=BBt,×BB=μ0ϵ0EEt,

where ϵ0=8.8541878176201012 (F/m) is the permittivity of free space, also known as the electric constant, and μ0=1.2566370614106 (H/m) is the permeability of free space, also known as the magnetic constant. Taking the curl of the two last equations and using the mathematical identity

×(×EE)=(EE)2EE=2EE when EE=0,

gives the wave equation governing the electric and magnetic field:

2EEt2=c22EE,
2BBt2=c22BB,

with c=1/μ0ϵ0 as the velocity of light. Each component of EE and BB fulfills a wave equation and can hence be solved independently.