In fluid dynamics, Janzen–Rayleigh expansion represents a regular perturbation expansion using the relevant mach number as the small parameter of expansion for the velocity field that possess slight compressibility effects. The expansion was first studied by O. Janzen in 1913 and Lord Rayleigh in 1916.
Steady potential flow Consider a steady potential flow that is characterized by the velocity potential φ ( x ) . {\displaystyle \varphi (\mathbf {x} ).} Then φ {\displaystyle \varphi } satisfies
( c 2 − φ x 2 ) φ x x + ( c 2 − φ y 2 ) φ y y + ( c 2 − φ z 2 ) φ z z − 2 ( φ x φ y φ x y + φ y φ z φ y z + φ z φ x ϕ z x ) = 0 {\displaystyle (c^{2}-\varphi _{x}^{2})\varphi _{xx}+(c^{2}-\varphi _{y}^{2})\varphi _{yy}+(c^{2}-\varphi _{z}^{2})\varphi _{zz}-2(\varphi _{x}\varphi _{y}\varphi _{xy}+\varphi _{y}\varphi _{z}\varphi _{yz}+\varphi _{z}\varphi _{x}\phi _{zx})=0}
where c = c ( v 2 ) {\displaystyle c=c(v^{2})} , the sound speed is expressed as a function of the velocity magnitude v 2 = ( ∇ φ ) 2 . {\displaystyle v^{2}=(\nabla \varphi )^{2}.} For a polytropic gas, we can write
c 2 = c 0 2 − γ − 1 2 v 2 {\displaystyle c^{2}=c_{0}^{2}-{\frac {\gamma -1}{2}}v^{2}}
where γ {\displaystyle \gamma } is the specific heat ratio, c 0 2 = h 0 ( γ − 1 ) / 2 {\displaystyle c_{0}^{2}=h_{0}(\gamma -1)/2} is the stagnation sound speed (i.e., the sound speed in a gas at rest) and h 0 {\displaystyle h_{0}} is the stagnation enthalpy. Let U {\displaystyle U} be the characteristic velocity scale and c 0 {\displaystyle c_{0}} is the characteristic value of the sound speed, then the function c ( v 2 ) {\displaystyle c(v^{2})} is of the form
c 2 U 2 = 1 M 2 − γ − 1 2 v 2 U 2 . {\displaystyle {\frac {c^{2}}{U^{2}}}={\frac {1}{M^{2}}}-{\frac {\gamma -1}{2}}{\frac {v^{2}}{U^{2}}}.}
where M = U / c 0 {\displaystyle M=U/c_{0}} is the relevant Mach number. For small Mach numbers, we can introduce the series
φ = U ( φ 0 + M 2 φ 1 + M 4 φ 2 + ⋯ ) {\displaystyle \varphi =U(\varphi _{0}+M^{2}\varphi _{1}+M^{4}\varphi _{2}+\cdots )}
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