Characteristics-Like Approach for Solving Hyperbolic Equation of First Order
Авторы: Синь Вэнь, Вяткин Александр Владимирович, Шайдуров Владимир Викторович
Рубрика: Математика
Опубликовано в Молодой учёный №3 (50) март 2013 г.
Библиографическое описание:
Синь В., Вяткин А. В., Шайдуров В. В. Characteristics-Like Approach for Solving Hyperbolic Equation of First Order // Молодой ученый. — 2013. — №3. — С. 5-12.
1. Introduction
We consider numerical solving the hyperbolic equation
equipped with suitable initial condition for known velocity coefficient
Among the successful numerical methods for solving this equation we mention such nonoscillatory conservative finite difference shemes as TVD (total variation diminishing), TVB (total variation bounded), and ENO (essentially nonoscillatory) ones (see, for example, [1]- [14] and the reference there).
In order to highlight the essential ingredients of suggested approach we begin with one-dimensional problem, keeping in mind that we shall extend these methods in subsequent papers. Moreover, for simplification we take periodic data to avoid a description complication for inessential issues connected with boundary-value conditions.
2. The statement of problem and the main theorem
with initial condition
Coefficient is given at and functions are supposed periodical in with period and are smooth enough for further considerations.
One of difficulties in solving (1)-(2) is that solution may contain discontinuities even for smooth data. But we start our considerations for the case of smooth solution.
For both these nodes we construct the characteristics of equation (1) at segment [16, 17]. They satisfy the ordinary differential equation with different initial values:
Fig. 1. Trajectories
These characteristics define two trajectories for in plane Each of these trajectories crosses line in some point We suppose that they are not mutually crossed and therefore
Theorem 1. For smooth solution of equation (1) we have equality
Proof. Define by the curvilinear quadrangle bounded by lines And define by the corresponding parts of these lines, which form the boundary (see Fig. 2). Introduce also the external normal defined at each part of boundary except 4 vertices of quadrangle.
Now use formula by Gauss-Ostrogradskii [16, 17] in the following form:
where sing means scalar product. Since the boundary consists of four parts we calculate the integral over separately on each line:
Fig. 2. Integration along boundary
Minus appeared in right-hand side because of opposite direction of integration. At arbitrary point the tangent vector is Therefore the external normal equals
Therefore we get
For other two parts of the boundary we use the same way to calculate the integrals and get
Combine (5) — (7) and (9) — (11):
It implies (4). □
3. Simple semi-discrete approximation
Now take integer and construct uniform mesh in with nodes and meshsize Let we know the (approximate) solution at time level and construct the approximate solution at time level Integrals of solution in a small vicinities of each point may be some useful intermediate data. For example, let construct integrals
For this purpose in the context of previous section we take two points and construct two trajectories These trajectories produce two points at time level Due to Theorem 1 we get
Fig. 3. Segment for partial integration on grid
But at previous level we know only integrals on segment which generally do not coincide with segment For example, let we have situation at level with some integer as in Fig. 3. So, we need to use some approximation of partial integrals.
The simple way consists in approximation of solution by piece-wise constant function. Thus we put
But this interpolation is rather rough. It gives accuracy of order only. Instead of it we take linear interpolation at each segment For this purpose at first we put
and then define
with period for This time we get interpolation accuracy of order
Of course the situation at initial level is simpler: we can use for example trapezoidal quadrature formula for any segment with accuracy
Therefore our numerical algorithm for solving problem (1) — (2) is as follows. Take integer and construct uniform mesh in with nodes and meshsize Then for make the following cycle supposing that the approximate solution is known yet at previous time-level for
1. With the help of values in these points and periodicity we construct the piecewise linear (periodical) interpolant
2. For each point construct trajectories down to time-level like in previous considerations. They produce cross-points If goes outside segment we use periodicity of our data.
by trapezoid quadrature formula separately at each nonempty subinterval where is linear.
3. Due to Theorem 1 it is supposed that
Therefore like in (15) — (16) we put
Thus, we complete our cycle which may be executed up to last time-level
Condensed form of this algorithm in terms of piecewise linear periodical interpolants is written as follows:
So, we get approximate discrete solution at each time-level First we prove the conservation law in discrete form.
Let a discrete function is given, and we construct piecewise linear interpolant with period 1.
Theorem 2. For any initial condition the approximate solution (17) — (20) satisfies the equality:
Proof. We prove this equality by induction in For this inequality is valid because of initial condition. Suppose that estimate (21) is valid for some and prove it for Indeed, because of (18) and (20) we get
Thus we prove
Now we prove a stability of algorithm (17) — (20) in the discrete norm analogous to that of space
Theorem 3. For any intermediate discrete function the solution of (17) — (20) satisfies the inequality:
Proof. Indeed, because of (18) and (20) we get
Let introduce the basis functions for linear interpolation
Then for piecewise linear interpolant we get
Then
Combine this inequality with (25) and (26) we get (24). □
Now evaluate an error of approximate solution in introduced discrete norm.
Theorem 4. For sufficiently smooth solution of problem (1) — (2) we have the following estimate for the constructed approximate solution:
Proof. We prove this inequality by induction in For this inequality is valid because of exact initial condition (2): Suppose that estimate (26) is valid for some and prove it for
Because of Taylor series in of in the vicinity of point we get equality
Because of Theorem 1
Instead of let use its piecewise linear periodical interpolant Then
Thus, we get equality
where values of are constructed by piecewise linear periodical interpolation.
Now let subtract (33) from (32), multiply its modulus by and sum for all
Due to Theorem 3 last terms in brackets is evaluated by Thus
Let put then this inequality is transformed with the help (29):
that is equivalent to (27). □
We can see that at last level we get inequality
In some sense we got a restriction on temporal meshsize to get convergence. For example, to get first order of convergence, it is enough to take
with any constant independent of But this restriction is not such strong up to constant as Courant — Friedrichs — Lewy (CFL) condition:
Moreover, it is opposite in meaning: here the greater the better accuracy.
Thus, this approach is convenient for the problems with huge velocity which come from a computational aerodynamics: we have computational stability on the base of Theorem 3 and conservation law on the base of Theorem 2.
4. Numerical experiment
Then exact solution is
The result of implementing the presented algorithm is given in Table 1 for several The first column of Table 1 expresses a relation / h (for most implemented values in computations) and the first string shows a number n of mesh nodes. Other entries contain the value
Table 1
n |
64 |
128 |
256 |
512 |
1024 |
2048 |
4 |
0,02358 |
0,01203 |
0,00608 |
0,00305 |
0,00153 |
0,00077 |
2 |
0,04536 |
0,02360 |
0,01204 |
0,00608 |
0,00305 |
0,00153 |
1 |
0,08423 |
0,04546 |
0,02362 |
0,01204 |
0,00608 |
0,00305 |
1 / 2 |
0,14610 |
0,08442 |
0,04548 |
0,02362 |
0,01204 |
0,00608 |
1 / 4 |
0,22493 |
0,14643 |
0,08446 |
0,04549 |
0,02362 |
0,01204 |
Thus we indeed have the first order of accuracy on h when / h is fixed.
5. Conclusion
Thus, we present the numerical approach which is more convenient for huge velocity then approaches listed in introduction. Of course, we stay some open questions like boundary condition instead of periodical one, nonlinear dependence of velocity on solution and other. Of course, we need to trace the effect of the approximate solving the characteristics equations instead of exact process. But we successively consider these issues in next publications, including generalization for two-dimensional and three-dimensional equations.
At first glance, this approach is some integral version of the characteristics method. Moreover, its accuracy is higher, the less time steps done in the algorithm. But in the future, we will apply it to the equations with nonzero right-hand side for the approximation of which a small time step will be crucial.
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