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[1] and Lord Rayleigh in 1916.[2]
Steady potential flow
Consider a steady potential flow that is characterized by the velocity potential  Then
 Then  satisfies
 satisfies
 
where  , the sound speed is expressed as a function of the velocity magnitude
, the sound speed is expressed as a function of the velocity magnitude  For a polytropic gas, we can write
 For a polytropic gas, we can write
 
where  is the specific heat ratio,
 is the specific heat ratio,  is the stagnation sound speed (i.e., the sound speed in a gas at rest) and
 is the stagnation sound speed (i.e., the sound speed in a gas at rest) and  is the stagnation enthalpy. Let
 is the stagnation enthalpy. Let  be the characteristic velocity scale and
 be the characteristic velocity scale and  is the characteristic value of the sound speed, then the function
 is the characteristic value of the sound speed, then the function  is of the form
 is of the form
 
where  is the relevant Mach number.
 is the relevant Mach number. 
For small Mach numbers, we can introduce the series[3]
 
Substituting this governing equation and collecting terms of different orders of  leads to a set of equations. These are
 leads to a set of equations. These are
 
and so on. Note that  is independent of
 is independent of  with which the latter quantity appears in the problem for
 with which the latter quantity appears in the problem for  .
.
Imai–Lamla method
A simple method for finding the particular integral for  in two dimensions was devised by Isao Imai and Ernst Lamla.[4][5][6] In two dimensions, the problem can be handled using complex analysis by introducing the complex potential
 in two dimensions was devised by Isao Imai and Ernst Lamla.[4][5][6] In two dimensions, the problem can be handled using complex analysis by introducing the complex potential  formally regarded as the function of
 formally regarded as the function of  and its conjugate
 and its conjugate  ; here
; here  is the stream function, defined such that
 is the stream function, defined such that
 
where  is some reference value for the density. The perturbation series of
 is some reference value for the density. The perturbation series of  is given by
 is given by
![{\displaystyle f(z,{\overline {z}})=U[f_{0}(z)+M^{2}f_{1}(z,{\overline {z}})+\cdots ]}](./_assets_/b6a5d5dc69f84c36c3746ba090c631af6a2b05f7.svg) 
where  is an analytic function since
 is an analytic function since  and
 and  , being solutions of the Laplace equation, are harmonic functions. The integral for the first-order problem leads to the Imai–Lamla formula[7][8]
, being solutions of the Laplace equation, are harmonic functions. The integral for the first-order problem leads to the Imai–Lamla formula[7][8]
 
where  is the homogeneous solution (an analytic function), that can be used to satisfy necessary boundary conditions. The series for the complex velocity potential
 is the homogeneous solution (an analytic function), that can be used to satisfy necessary boundary conditions. The series for the complex velocity potential  is given by
 is given by
![{\displaystyle g(z,{\overline {z}})=U[g_{0}(z)+M^{2}g_{1}(z,{\overline {z}})+\cdots ]}](./_assets_/9671d37fc801222d02fec8d9a4f0ec1dc9a24f55.svg) 
where  and[9]
 and[9]
 
References
- ^ O. Janzen, Beitrag zu einer Theorie der stationären Strömung kompressibler Flüssigkeiten. Phys. Zeits., 14 (1913)
- ^ Rayleigh, L. (1916). I. On the flow of compressible fluid past an obstacle. The London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science, 32(187), 1-6.
- ^ Von Karman, Th. "Compressibility effects in aerodynamics." Journal of spacecraft and rockets 40, no. 6 (1941): 992-1011.
- ^ IMAI, Isao. "A new method of successive approximations for dealing with the two-dimensional subsonic flow of a compressible fluid." Proceedings of the Physico-Mathematical Society of Japan. 3rd Series 24 (1942): 120-129.
- ^ Lamla, E. (1942). On the symmetrical potential flow of compressible fluid past a circular cylinder in the tunnel in the subcritical zone (No. NACA-TM-1018).
- ^ Imai, Isao, and Takasi Aihara. On the subsonic flow of a compressible fluid past an elliptic cylinder. Aeronautical Research Institute, Tokyo Imperial University, 1940.
- ^ JACOB, C. 1959 Introduction Mathématique a la Mécanique des Fluides. Gauthier-Villars.
- ^ Barsony-Nagy, A. "Extension of the Blasius force theorem to subsonic speeds." AIAA journal 23, no. 11 (1985): 1811-1812.
- ^ Carabineanu, Adrian. "A boundary integral equations approach for the study of the subsonic compressible flow past a cusped airfoil." Nonlinear Analysis: Theory, Methods & Applications 30, no. 6 (1997): 3449-3454.