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This research presents a novel method for Mannheim curves in three-dimensional Galilean space G3. Using this method, the necessary and sufficient conditions, along with the established results, must be satisfied for a curve in G3 to qualify as a Mannheim curve. Furthermore, relevant examples and graphs are provided to demonstrate how Mannheim curves and their partners can correspond to Salkowski and anti-Salkowski curves. Finally, in G3, the Mannheim partner curves are described.
Citation: Mervat Elzawy, Safaa Mosa. A novel method for Mannheim curves in the Galilean 3−space G3[J]. AIMS Mathematics, 2024, 9(11): 31239-31251. doi: 10.3934/math.20241506
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This research presents a novel method for Mannheim curves in three-dimensional Galilean space G3. Using this method, the necessary and sufficient conditions, along with the established results, must be satisfied for a curve in G3 to qualify as a Mannheim curve. Furthermore, relevant examples and graphs are provided to demonstrate how Mannheim curves and their partners can correspond to Salkowski and anti-Salkowski curves. Finally, in G3, the Mannheim partner curves are described.
The study of nonlinear systems of singular initial value problems has recently attracted many mathematicians and physicists [1,2,3,4,5,6,7,8,9,10,11,12]. One of the systems in this category is the following Lane-Emden system of the form:
d2ω1(τ)dτ2+δ1τdω1(τ)dτ+ℏ1(ω1(τ),ω2(τ))=ℵ1(τ), | (1) |
d2ω1(τ)dτ2+δ1τdω1(τ)dτ+ℏ1(ω1(τ),ω2(τ))=ℵ1(τ), |
subject to
ω1(0)=ε1,ω'1(0)=0, | (2) |
ω2(0)=ϑ1,ω'2(0)=0, |
where
Recently, modeling a variety of physical and chemical phenomena, including chemical reactions, population evolution, and pattern formation leads to the system of Lane-Emden equations [7]. Therefore, numerous approaches have been proposed for the solutions of scalar and system of Lane-Emden equations [1,2,10,11,12,12,13,14,15,17,18,42,43,44,45,46,47].
Spline methods employing piecewise polynomial functions have been demonstrated to be convenient methods for obtaining numerical solutions to many challenging models in science, engineering, and mathematics due to their simplicity of implementation and efficiency [29,30,31,32,33,34]. One of the well-known spline methods is the so-called B-spline (the "B" stands for basis) functions, which were first proposed by Schoenberg in 1946. The B-spline functions [35,36] have recently been a valuable tool in numerical computation, approximation theory, and image processing as they have various useful properties such as numerical stability of computations, local effects of coefficient changes, and built-in smoothness between neighboring polynomial pieces. The degrees of B-spline and the collocation points are the main factors that play a significant role in the execution of the technique and affect the outcomes to be achieved up to a required level of accuracy.
One of the most efficient and versatile techniques for obtaining approximate solutions is the cubic B-spline method (CBSM). The CBSM is a third-order piecewise polynomial constructed from a combination of recursive formulas referred to as the cubic B-spline basis. The derivation of the B-spline basis and the construction of the B-spline function are thoroughly discussed in [37,38]. In recent years, the CBSM has been successfully applied to various mathematical problems [39]. This demonstrates the effectiveness and usefulness of spline approaches through their numerous successful implementations. Therefore, this paper investigates the approximate solution of systems of the Lane-Emden equations using the CBSM.
This paper is organized as follows, in the next section, we present the basic preliminaries of the method. A short summary of cubic B-Spline method is presented in Section 3. We show the convergence analysis in Section 4. Finally, we present some numerical examples in Section 5.
In this section, we introduce some basic facts regarding cubic B-spline approximation. Assume that the interval
τi=α+iΛ,i=0,⋯,k, |
where
Λ=(β−α)/k. |
The linear space of the cubic spline over the given partition is
M3(I)={μ(τ)∈C2(I):μ(τ)|Ii∈P3,i=0,...,k−1}, |
where
−Γ=[α−3Λ,β+3Λ] |
with the equidistant knots
τi=α+iΛ,i=−3,...,k+3. |
The cubic B-spline function
Ki(τ),i=−1,...,k+1, |
is given by [40]
Ki(τ)={(τ−τi)36Λ3,τ∈[τi,τi+1],(τ−τi)36Λ3−2(τ−τi+1)33Λ3,τ∈[τi+1,τi+2],(τi+4−τ)36Λ3−2(τi+3−τ)33Λ3,τ∈[τi+2,τi+3],(τi+4−τ)36Λ3,τ∈[τi+3,τi+4],0,else. |
The
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For a sufficiently smooth function
μ(τi)=ρ(τi),i=0,...,k, |
and
μ'(α)=ρ'(α), |
such that
μ(τ)=k+1∑i=−1λiKi(τ), | (3) |
where
Using (3), we get
μ(τj)=k+1∑i=−1λiKi(τj)=λj−1+4λj+λj+16, | (4) |
μ'(τj)=k+1∑i=−1λiK'i(τj)=λj+1−λj−12Λ, | (5) |
μ''(τj)=k+1∑i=−1λiK''i(τj)=λj−1−2λj+λj+1Λ2. | (6) |
Equations (4)–(6) are the most important relations in deriving the CBSM.
In this section, we present the cubic B-spline method for (1) and (2). Let
μ1(τ)=k+1∑i=−1λiKi(τ) |
and
μ2(τ)=k+1∑i=−1ηiKi(τ) |
denote the approximate solutions of system (1) and (2) of
{(1+δ1)d2ω1(τ)dτ2+ℏ1(ω1(τ),ω2(τ))=ℵ1(τ),(1+δ2)d2ω2(τ)dτ2+ℏ2(ω1(τ),ω2(τ))=ℵ2(τ),forτ=0,{d2ω1(τ)dτ2+δ1τdω1(τ)dτ+ℏ1(ω1(τ),ω2(τ))=ℵ1(τ),d2ω2(τ)dτ2+δ2τdω2(τ)dτ+ℏ2(ω1(τ),ω2(τ))=ℵ2(τ),forτ≠0. | (7) |
By discretizing (7), we get
{(1+δ1)d2ω1(τ0)dτ2+ℏ1(ω1(τ0),ω2(τ0))=ℵ1(τ0),(1+δ2)d2ω2(τ0)dτ2+ℏ2(ω1(τ0),ω2(τ0))=ℵ2(τ0),{d2ω1(τj)dτ2+δ1τjdω1(τj)dτ+ℏ1(ω1(τj),ω2(τj))=ℵ1(τj),d2ω2(τj)dτ2+δ2τjdω2(τj)dτ+ℏ2(ω1(τj),ω2(τj))=ℵ2(τj), | (8) |
where
{(1+δ1)(λ−1−2λ0+λ1Λ2)+ℏ1(ε1,ϑ1)=ℵ1(τ0),(1+δ2)(η−1−2η0+η1Λ2)+ℏ2(ε1,ϑ1)=ℵ2(τ0), |
{(λi−1−2λi+λi+1Λ2)+δ1τj(λj+1−λj−12Λ)+ℏ1(λi−1+4λi+λi+16,ηi−1+4ηi+ηi+16)=ℵ1(τj),j=1,⋯,k,(ηi−1−2ηi+ηi+1Λ2)+δ2τj(ηj+1−ηj−12Λ)+ℏ2(λi−1+4λi+λi+16,ηi−1+4ηi+ηi+16)=ℵ2(τj),j=1,⋯,k. | (9) |
The initial conditions (2) as well provide the following four equations
ω1(0)=ε1=λ−1+4λ0+λ16, | (10) |
ω'1(0)=0=λ1−λ−12Λ, | (11) |
ω2(0)=ϑ1=η−1+4η0+η16, | (12) |
ω''2(0)=0=η1−η−12Λ. | (13) |
Equations (9)–(13) give us
μ1(τ)=k+1∑i=−1λiKi(τ) |
and
μ2(τ)=k+1∑i=−1ηiKi(τ). |
In this section, we analyze the convergence for the proposed method. For this purpose, we assume
Λ[μ'j(τi−1)+4μ'j(τi)+μ'j(τi+1)]=3[ωj(τi+1)−ωj(τi−1)], | (14) |
Λ2μ''j(τi)=6[μj(τi+1)−μj(τi)]−2Λ[2μ'j(τi)+μ'j(τi+1)], | (15) |
Λ6(E−1+4+E)μ'j(τi)=12(E−E−1)ωj(τi), | (16) |
eΛD+e−ΛD=2∞∑k=0(ΛD)2k(2k)!,eΛD−e−ΛD=2∞∑k=0(ΛD)2k+1(2k+1)!. | (17) |
Therefore, using (17), (16) can be expressed as
(1+13∞∑k=1(ΛD)2k(2k)!)μ'j(τi)=(∞∑k=0(ΛD)2k+1(2k+1)!)ωj(τi). | (18) |
Simplifying (18) gives
μ'j(τi)=(∞∑k=0(ΛD)2k+1(2k+1)!)(1+13∞∑k=1(ΛD)2k(2k)!)−1ωj(τi) = (D+Λ2D33!+Λ4D55!+⋯)(1−(Λ2D26+Λ4D472+⋯)+(Λ2D26+Λ4D472+⋯)2+⋯)ωj(τi)=D(1−Λ4D4180+Λ6D61512−⋯)ωj(τi). | (19) |
Therefore,
μ'j(τi)=ω'j(τi)−Λ4180ω(5)j(τi)+⋯. | (20) |
Similarly, (15) gives
μ''j(τi)=ω''j(τi)−112Λ2ω(4)j(τi)+1360Λ4ω(6)j(τi)+O(Λ6), | (21) |
At this point, the error functions
e1(τi)=ℵ1(τj)−d2ω1(τj)dτ2−δ1τjdω1(τj)dτ−ℏ1(ω1(τj),ω2(τj))=d2μ1(τj)dτ2+δ1τjdμ1(τj)dτ+ℏ1(μ1(τj),μ2(τj))−d2ω1(τj)dτ2−δ1τjdω1(τj)dτ−ℏ1(ω1(τj),ω2(τj))=[d2μ1(τj)dτ2−d2ω1(τj)dτ2]+δ1τj[dμ1(τj)dτ−dω1(τj)dτ],e2(τi)=ℵ2(τj)−d2ω2(τj)dτ2−δ2τjdω2(τj)dτ−ℏ2(ω1(τj),ω2(τj))=d2μ2(τj)dτ2+δ2τjdμ2(τj)dτ+ℏ2(μ1(τj),μ2(τj))−d2ω2(τj)dτ2−δ2τjdω2(τj)dτ−ℏ2(ω1(τj),ω2(τj))=[d2μ2(τj)dτ2−d2ω2(τj)dτ2]+δ2τj[dμ2(τj)dτ−dω2(τj)dτ], | (22) |
where
{‖{e}_{1}\left({\tau }_{i}\right)‖}_{{\mathrm{\infty }}} = O\left({{\mathrm{\Lambda }}}^{2}\right), |
{‖{e}_{2}\left({\tau }_{i}\right)‖}_{{\mathrm{\infty }}} = O\left({{\mathrm{\Lambda }}}^{2}\right). | (23) |
For i = 0, we get
{e}_{1}\left({\tau }_{0}\right) = {\aleph }_{1}\left({\tau }_{0}\right)-\left(1+{\delta }_{1}\right)\frac{{d}^{2}{\omega }_{1}\left({\tau }_{0}\right)}{d{\tau }^{2}}-{\hslash }_{1}\left({\omega }_{1}\left({\tau }_{0}\right),{\omega }_{2}\left({\tau }_{0}\right)\right)\\ = \left(1+{\delta }_{1}\right)\frac{{d}^{2}{\mu }_{1}\left({\tau }_{0}\right)}{d{\tau }^{2}}+{\hslash }_{1}\left({\mu }_{1}\left({\tau }_{0}\right),{\mu }_{2}\left({\tau }_{0}\right)\right)\\-\left(1+{\delta }_{1}\right)\frac{{d}^{2}{\omega }_{1}\left({\tau }_{0}\right)}{d{\tau }^{2}}-{\hslash }_{1}({\omega }_{1}\left({\tau }_{0}\right),{\omega }_{2}\left({\tau }_{0}\right)\\ = \left(1+{\delta }_{1}\right)\left[\frac{{d}^{2}{\mu }_{1}\left({\tau }_{0}\right)}{d{\tau }^{2}}-\frac{{d}^{2}{\omega }_{1}\left({\tau }_{0}\right)}{d{\tau }^{2}}\right],\\{e}_{2}\left({\tau }_{0}\right) = {\aleph }_{2}\left({\tau }_{0}\right)-(1+{\delta }_{2})\frac{{d}^{2}{\omega }_{2}\left({\tau }_{0}\right)}{d{\tau }^{2}}-{\hslash }_{2}({\omega }_{1}\left({\tau }_{0}\right),{\omega }_{2}\left({\tau }_{0}\right)) \\ = \left(1+{\delta }_{2}\right)\frac{{d}^{2}{\omega }_{2}\left({\tau }_{0}\right)}{d{\tau }^{2}}+{\hslash }_{2}\left({\mu }_{1}\left({\tau }_{0}\right),{\mu }_{2}\left({\tau }_{0}\right)\right)\\ -\left(1+{\delta }_{2}\right)\frac{{d}^{2}{\omega }_{2}\left({\tau }_{0}\right)}{d{\tau }^{2}}-{\hslash }_{1}({\omega }_{1}\left({\tau }_{0}\right),{\omega }_{2}\left({\tau }_{0}\right)\\ = (1+{\delta }_{2})\left[\frac{{d}^{2}{\omega }_{2}\left({\tau }_{0}\right)}{d{\tau }^{2}}-\frac{{d}^{2}{\omega }_{2}\left({\tau }_{0}\right)}{d{\tau }^{2}}\right]. | (24) |
Using (21) in (24), we have
{‖{e}_{1}\left({\tau }_{0}\right)‖}_{{\mathrm{\infty }}} = O\left({{\mathrm{\Lambda }}}^{2}\right),\\{‖{e}_{2}\left({\tau }_{0}\right)‖}_{{\mathrm{\infty }}} = O\left({{\mathrm{\Lambda }}}^{2}\right). | (25) |
Therefore, from (23) and (25), the truncation error for the considered system is
In this section, we present the numerical solution to (1) and (2) using the cubic B-spline technique. Several problems are examined to prove the accuracy and efficiency of the proposed method using the absolute errors between the approximate solutions and the exact solutions (
Problem 1. Consider the following system [24]
\frac{{d}^{2}{\omega }_{1}\left(\tau \right)}{d{\tau }^{2}}+\frac{3}{\tau }\frac{d{\omega }_{1}\left(\tau \right)}{d\tau }-4({\omega }_{1}\left(\tau \right)+{\omega }_{2}\left(\tau \right)) = 0,\\\frac{{d}^{2}{\omega }_{2}\left(\tau \right)}{d{\tau }^{2}}+\frac{2}{\tau }\frac{d{\omega }_{2}\left(\tau \right)}{d\tau }+3({\omega }_{1}\left(\tau \right)+{\omega }_{2}\left(\tau \right)) = 0, | (26) |
subject to
{\omega }_{1}\left(0\right) = 1,{\omega }_{1}^{{\text{'}}}\left(0\right) = 0,\\{\omega }_{2}\left(0\right) = 1,{\omega }_{2}^{{\text{'}}}\left(0\right) = 0, | (27) |
where the exact solutions are
1 | ||||||
1.01 | 0.99 | 0.99 | ||||
1.04 | 0.96 | 0.96 | ||||
1.09 | 0.91 | 0.91 | ||||
1.16 | 1.16 | 0.84 | 0.84 | |||
1.25 | 1.25 | 0.75 | 0.75 | |||
1.36 | 1.36 | 0.64 | 0.64 | |||
1.49 | 1.49 | 0.51 | 0.51 | |||
1.61 | 1.61 | 0.36 | 0.36 | |||
1.81 | 1.81 | 0.19 | 0.19 | |||
2 | 2 | 0 | 5.64363 |
Problem 2. Consider the following system [27]
{\omega }_{1}^{{\text{'}}{\text{'}}}\left(\tau \right)+\frac{2}{\tau }{\omega }_{1}^{{\text{'}}}\left(\tau \right)-\left(4{\tau }^{2}+6\right){\omega }_{1}\left(\tau \right)+{\omega }_{2}\left(\tau \right) = {\tau }^{4}-{\tau }^{3},\\{\omega }_{2}^{{\text{'}}{\text{'}}}\left(\tau \right)+\frac{8}{\tau }{\omega }_{2}^{{\text{'}}}\left(\tau \right)+{\omega }_{1}\left(\tau \right)+\tau {\omega }_{2}\left(\tau \right) = {e}^{{\tau }^{2}}+{\tau }^{5}-{\tau }^{4}+44{\tau }^{2}-30\tau , | (28) |
subject to
{\omega }_{1}\left(0\right) = 1,{\omega }_{1}^{{\text{'}}}\left(0\right) = 0,\\{\omega }_{2}\left(0\right) = 0,{\omega }_{2}^{{\text{'}}}\left(0\right) = 0, | (29) |
where the exact solutions are
{\omega }_{1}\left(\tau \right) = {e}^{{\tau }^{2}} |
and
{\omega }_{2}\left(\tau \right) = {\tau }^{4}-{\tau }^{3}. |
The obtained numerical and exact solutions, with different values of
1.09417 | |||||
1.17351 | 1.17389 | ||||
1.28403 | 1.2847 | ||||
1.43333 | 1.43446 | ||||
1.63232 | 1.63419 | ||||
1.89648 | 1.89952 | ||||
2.24791 | 2.25281 | ||||
2.71828 | 2.72617 |
0.0 | 0 | 0 | 0 | ||
0.1 | |||||
0.2 | |||||
-0.0189 | |||||
-0.0384 | |||||
-0.0625 | |||||
-0.0864 | |||||
-0.1029 | |||||
-0.1024 | |||||
-0.0729 | |||||
0 |
CBSM |
||
CBSM |
||
[27] (N=5) | ||
[27] (N=6) |
Problem 3. Consider the following system [24,41]
{\omega }_{1}^{{\text{'}}{\text{'}}}\left(\tau \right)+\frac{5}{\tau }{\omega }_{1}^{{\text{'}}}\left(\tau \right)+8({e}^{{\omega }_{1}\left(\tau \right)}+2{e}^{-\frac{{\omega }_{2}\left(\tau \right)}{2}}) = 0,\\ {\omega }_{2}^{{\text{'}}{\text{'}}}\left(\tau \right)+\frac{3}{\tau }{\omega }_{2}^{{\text{'}}}\left(\tau \right)-8({e}^{\frac{{\omega }_{1}\left(\tau \right)}{2}}+{e}^{-{\omega }_{2}\left(\tau \right)}) = 0, | (30) |
subject to
{\omega }_{1}\left(0\right) = 1-2{\mathrm{ln}}\left(2\right),{\omega }_{1}^{{\text{'}}}\left(0\right) = 0,\\{\omega }_{2}\left(0\right) = 1+2{\mathrm{ln}}\left(2\right),{\omega }_{2}^{{\text{'}}}\left(0\right) = 0, | (31) |
where the exact solutions are
{\omega }_{1}\left(\tau \right) = 1-2{\mathrm{ln}}({\tau }^{2}+2) |
and
{\omega }_{2}\left(\tau \right) = 1+2{\mathrm{ln}}({\tau }^{2}+2). |
We depicted our numerical and exact solutions with different values of
2.38629 | 2.38629 | 2.38629 | |||
2.39627 | 2.39625 | 2.39627 | |||
2.4259 | 2.42587 | 2.42599 | |||
2.47433 | 2.47427 | 2.47433 | |||
2.54022 | 2.54014 | 2.54022 | |||
2.62186 | 2.62176 | 2.62186 | |||
2.71732 | 2.71721 | 2.71732 | |||
2.82457 | 2.82445 | 2.82456 | |||
2.94156 | 2.94145 | 2.94156 | |||
3.06637 | 3.06628 | 3.06637 | |||
3.19722 | 3.19716 | 3.19722 |
CBSM |
||
CBSM |
||
[41] (j=3) | ||
[41] (j=4) |
Problem 4. Consider the following system of LEE [24,27,40,41]
{\omega }_{1}^{{\text{'}}{\text{'}}}\left(\tau \right)+\frac{1}{\tau }{\omega }_{1}^{{\text{'}}}\left(\tau \right)-{\omega }_{2}^{3}\left(\tau \right)({\omega }_{1}^{2}+1) = 0,\\{\omega }_{2}^{{\text{'}}{\text{'}}}\left(\tau \right)+\frac{3}{\tau }{\omega }_{2}^{{\text{'}}}\left(\tau \right)+{\omega }_{2}^{5}\left(\tau \right)({\omega }_{1}^{2}+3) = 0, | (32) |
subject to
{\omega }_{1}\left(0\right) = 1,{{\omega }^{{\text{'}}}}_{1}\left(0\right) = 0,\\{\omega }_{2}\left(0\right) = 1,{{\omega }^{{\text{'}}}}_{2}\left(0\right) = 0, | (33) |
where the exact solutions are
{\omega }_{1}\left(\tau \right) = \sqrt{{1+\tau }^{2}} |
and
{\omega }_{2}\left(\tau \right) = \frac{1}{\sqrt{{1+\tau }^{2}}}. |
The achieved numerical results with
1 | 1 | 0 | 1 | 0 | |
1.004988 | 1.004978 | 1.004987 | |||
1.019804 | 1.019776 | 1.019804 | |||
1.044031 | 1.043979 | 1.04403 | |||
1.077033 | 1.076957 | 1.077032 | |||
1.118034 | 1.117936 | 1.118033 | |||
1.16619 | 1.166076 | 1.166189 | |||
1.220656 | 1.220531 | 1.220654 | |||
1.280625 | 1.280495 | 1.280624 | |||
1.345362 | 1.34523 | 1.345361 | |||
1.414214 | 1.414079 | 1.414212 |
1 | 1 | 0 | 1 | ||
0.995037 | 0.995059 | 0.995037 | |||
0.980581 | 0.980623 | 0.980581 | |||
0.957826 | 0.957887 | 0.957827 | |||
0.928477 | 0.928545 | 0.928477 | |||
0.894427 | 0.894487 | 0.894428 | |||
0.857493 | 0.857525 | 0.857493 | |||
0.819232 | 0.819223 | 0.819232 | |||
0.780869 | 0.780811 | 0.780868 | |||
0.743294 | 0.743188 | 0.743293 | |||
0.707107 | 0.706957 | 0.707105 |
CBSM |
||
CBSM |
||
[27] (N=4) | ||
[27] (N=5) | ||
[40] (n=4) | ||
[41] (j=3) | ||
[41] (j=4) |
Problem 5. Consider the following system of LEE [24,40]
{\omega }_{1}^{{\text{'}}{\text{'}}}+\frac{8}{\tau }{\omega }_{1}^{{\text{'}}}\left(\tau \right)+(18{\omega }_{1}\left(\tau \right)-4{\omega }_{1}\left(\tau \right){\mathrm{ln}}{\omega }_{2}\left(\tau \right)) = 0,\\{\omega }_{2}^{{\text{'}}{\text{'}}}\left(\tau \right)+\frac{4}{\tau }{\omega }_{2}^{{\text{'}}}\left(\tau \right)+(4{\omega }_{2}\left(\tau \right){\mathrm{ln}}{\omega }_{1}\left(\tau \right)-10{\omega }_{2}\left(\tau \right)) = 0, | (34) |
subject to
{\omega }_{1}\left(0\right) = 1,{\omega }_{1}^{{\text{'}}}\left(0\right) = 0, \\ {\omega }_{2}\left(0\right) = 1,{\omega }_{2}^{{\text{'}}}\left(0\right) = 0, | (35) |
where the exact solutions are
Figure 4 represents the plot of our numerical and exact solutions for Problem 5 with different values of
1 | 1 | 0 | 1 | 0 | |
0.99005 | 0.990073 | 0.99005 | |||
0.960789 | 0.960817 | 0.96079 | |||
0.913931 | 0.913979 | 0.913932 | |||
0.852144 | 0.85221 | 0.852144 | |||
0.778801 | 0.778879 | 0.778802 | |||
0.697676 | 0.697756 | 0.697677 | |||
0.612626 | 0.612695 | 0.612627 | |||
0.527292 | 0.527337 | 0.527293 | |||
0.444858 | 0.444871 | 0.444858 | |||
0.367879 | 0.367856 | 0.367879 |
1 | 1 | 0 | 1 | 0 | |
1.01005 | 1.010078 | 1.01005 | |||
1.040811 | 1.040871 | 1.040811 | |||
1.094174 | 1.094299 | 1.094175 | |||
1.173511 | 1.173751 | 1.173513 | |||
1.284025 | 1.284458 | 1.284029 | |||
1.433329 | 1.434077 | 1.433337 | |||
1.632316 | 1.633578 | 1.632328 | |||
1.896481 | 1.898582 | 1.896501 | |||
2.247908 | 2.251381 | 2.247942 | |||
2.718282 | 2.724006 | 2.718338 |
CBSM |
||
CBSM |
||
[40] (n=4) | ||
[41] (j=3) | ||
[41] (j=4) |
The system of Lane-Emden type equations describes a variety of phenomena in theoretical physics, star structure, and astrophysics. In this study, we introduce and examine the use of the cubic B-spline method for studying the solution of singular and nonlinear systems of Lane-Emden equations. To address the singularity that occurs at τ = 0, we use L'Hôpital's rule. We also evaluate the accuracy and validity of the proposed technique, demonstrating its success in solving the considered system. The presented test problems have shown the simplicity and applicability of the proposed method. We provide tabular and graphical representations to confirm its effectiveness, observing that our numerical solutions are in good agreement with the exact solutions. It is observed that our numerical solutions are in good agreement with the exact ones. Furthermore, we show that by decreasing the mesh size, the numerical results converge to the analytical solution, which confirms the convergence of the algorithm. It is noteworthy that the CPU time of the proposed method for each evaluated problem is under 1 second.
The authors express their gratitude to the dear referees, who wish to remain anonymous and the editor for their helpful suggestions, which improved the final version of this paper.
The authors declare no conflicts of interest.
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else | ||||
0 | ||||
0 | ||||
0 |
1 | ||||||
1.01 | 0.99 | 0.99 | ||||
1.04 | 0.96 | 0.96 | ||||
1.09 | 0.91 | 0.91 | ||||
1.16 | 1.16 | 0.84 | 0.84 | |||
1.25 | 1.25 | 0.75 | 0.75 | |||
1.36 | 1.36 | 0.64 | 0.64 | |||
1.49 | 1.49 | 0.51 | 0.51 | |||
1.61 | 1.61 | 0.36 | 0.36 | |||
1.81 | 1.81 | 0.19 | 0.19 | |||
2 | 2 | 0 | 5.64363 |
1.09417 | |||||
1.17351 | 1.17389 | ||||
1.28403 | 1.2847 | ||||
1.43333 | 1.43446 | ||||
1.63232 | 1.63419 | ||||
1.89648 | 1.89952 | ||||
2.24791 | 2.25281 | ||||
2.71828 | 2.72617 |
0.0 | 0 | 0 | 0 | ||
0.1 | |||||
0.2 | |||||
-0.0189 | |||||
-0.0384 | |||||
-0.0625 | |||||
-0.0864 | |||||
-0.1029 | |||||
-0.1024 | |||||
-0.0729 | |||||
0 |
CBSM |
||
CBSM |
||
[27] (N=5) | ||
[27] (N=6) |
2.38629 | 2.38629 | 2.38629 | |||
2.39627 | 2.39625 | 2.39627 | |||
2.4259 | 2.42587 | 2.42599 | |||
2.47433 | 2.47427 | 2.47433 | |||
2.54022 | 2.54014 | 2.54022 | |||
2.62186 | 2.62176 | 2.62186 | |||
2.71732 | 2.71721 | 2.71732 | |||
2.82457 | 2.82445 | 2.82456 | |||
2.94156 | 2.94145 | 2.94156 | |||
3.06637 | 3.06628 | 3.06637 | |||
3.19722 | 3.19716 | 3.19722 |
CBSM |
||
CBSM |
||
[41] (j=3) | ||
[41] (j=4) |
1 | 1 | 0 | 1 | 0 | |
1.004988 | 1.004978 | 1.004987 | |||
1.019804 | 1.019776 | 1.019804 | |||
1.044031 | 1.043979 | 1.04403 | |||
1.077033 | 1.076957 | 1.077032 | |||
1.118034 | 1.117936 | 1.118033 | |||
1.16619 | 1.166076 | 1.166189 | |||
1.220656 | 1.220531 | 1.220654 | |||
1.280625 | 1.280495 | 1.280624 | |||
1.345362 | 1.34523 | 1.345361 | |||
1.414214 | 1.414079 | 1.414212 |
1 | 1 | 0 | 1 | ||
0.995037 | 0.995059 | 0.995037 | |||
0.980581 | 0.980623 | 0.980581 | |||
0.957826 | 0.957887 | 0.957827 | |||
0.928477 | 0.928545 | 0.928477 | |||
0.894427 | 0.894487 | 0.894428 | |||
0.857493 | 0.857525 | 0.857493 | |||
0.819232 | 0.819223 | 0.819232 | |||
0.780869 | 0.780811 | 0.780868 | |||
0.743294 | 0.743188 | 0.743293 | |||
0.707107 | 0.706957 | 0.707105 |
CBSM |
||
CBSM |
||
[27] (N=4) | ||
[27] (N=5) | ||
[40] (n=4) | ||
[41] (j=3) | ||
[41] (j=4) |
1 | 1 | 0 | 1 | 0 | |
0.99005 | 0.990073 | 0.99005 | |||
0.960789 | 0.960817 | 0.96079 | |||
0.913931 | 0.913979 | 0.913932 | |||
0.852144 | 0.85221 | 0.852144 | |||
0.778801 | 0.778879 | 0.778802 | |||
0.697676 | 0.697756 | 0.697677 | |||
0.612626 | 0.612695 | 0.612627 | |||
0.527292 | 0.527337 | 0.527293 | |||
0.444858 | 0.444871 | 0.444858 | |||
0.367879 | 0.367856 | 0.367879 |
1 | 1 | 0 | 1 | 0 | |
1.01005 | 1.010078 | 1.01005 | |||
1.040811 | 1.040871 | 1.040811 | |||
1.094174 | 1.094299 | 1.094175 | |||
1.173511 | 1.173751 | 1.173513 | |||
1.284025 | 1.284458 | 1.284029 | |||
1.433329 | 1.434077 | 1.433337 | |||
1.632316 | 1.633578 | 1.632328 | |||
1.896481 | 1.898582 | 1.896501 | |||
2.247908 | 2.251381 | 2.247942 | |||
2.718282 | 2.724006 | 2.718338 |
CBSM |
||
CBSM |
||
[40] (n=4) | ||
[41] (j=3) | ||
[41] (j=4) |
else | ||||
0 | ||||
0 | ||||
0 |
1 | ||||||
1.01 | 0.99 | 0.99 | ||||
1.04 | 0.96 | 0.96 | ||||
1.09 | 0.91 | 0.91 | ||||
1.16 | 1.16 | 0.84 | 0.84 | |||
1.25 | 1.25 | 0.75 | 0.75 | |||
1.36 | 1.36 | 0.64 | 0.64 | |||
1.49 | 1.49 | 0.51 | 0.51 | |||
1.61 | 1.61 | 0.36 | 0.36 | |||
1.81 | 1.81 | 0.19 | 0.19 | |||
2 | 2 | 0 | 5.64363 |
1.09417 | |||||
1.17351 | 1.17389 | ||||
1.28403 | 1.2847 | ||||
1.43333 | 1.43446 | ||||
1.63232 | 1.63419 | ||||
1.89648 | 1.89952 | ||||
2.24791 | 2.25281 | ||||
2.71828 | 2.72617 |
0.0 | 0 | 0 | 0 | ||
0.1 | |||||
0.2 | |||||
-0.0189 | |||||
-0.0384 | |||||
-0.0625 | |||||
-0.0864 | |||||
-0.1029 | |||||
-0.1024 | |||||
-0.0729 | |||||
0 |
CBSM |
||
CBSM |
||
[27] (N=5) | ||
[27] (N=6) |
2.38629 | 2.38629 | 2.38629 | |||
2.39627 | 2.39625 | 2.39627 | |||
2.4259 | 2.42587 | 2.42599 | |||
2.47433 | 2.47427 | 2.47433 | |||
2.54022 | 2.54014 | 2.54022 | |||
2.62186 | 2.62176 | 2.62186 | |||
2.71732 | 2.71721 | 2.71732 | |||
2.82457 | 2.82445 | 2.82456 | |||
2.94156 | 2.94145 | 2.94156 | |||
3.06637 | 3.06628 | 3.06637 | |||
3.19722 | 3.19716 | 3.19722 |
CBSM |
||
CBSM |
||
[41] (j=3) | ||
[41] (j=4) |
1 | 1 | 0 | 1 | 0 | |
1.004988 | 1.004978 | 1.004987 | |||
1.019804 | 1.019776 | 1.019804 | |||
1.044031 | 1.043979 | 1.04403 | |||
1.077033 | 1.076957 | 1.077032 | |||
1.118034 | 1.117936 | 1.118033 | |||
1.16619 | 1.166076 | 1.166189 | |||
1.220656 | 1.220531 | 1.220654 | |||
1.280625 | 1.280495 | 1.280624 | |||
1.345362 | 1.34523 | 1.345361 | |||
1.414214 | 1.414079 | 1.414212 |
1 | 1 | 0 | 1 | ||
0.995037 | 0.995059 | 0.995037 | |||
0.980581 | 0.980623 | 0.980581 | |||
0.957826 | 0.957887 | 0.957827 | |||
0.928477 | 0.928545 | 0.928477 | |||
0.894427 | 0.894487 | 0.894428 | |||
0.857493 | 0.857525 | 0.857493 | |||
0.819232 | 0.819223 | 0.819232 | |||
0.780869 | 0.780811 | 0.780868 | |||
0.743294 | 0.743188 | 0.743293 | |||
0.707107 | 0.706957 | 0.707105 |
CBSM |
||
CBSM |
||
[27] (N=4) | ||
[27] (N=5) | ||
[40] (n=4) | ||
[41] (j=3) | ||
[41] (j=4) |
1 | 1 | 0 | 1 | 0 | |
0.99005 | 0.990073 | 0.99005 | |||
0.960789 | 0.960817 | 0.96079 | |||
0.913931 | 0.913979 | 0.913932 | |||
0.852144 | 0.85221 | 0.852144 | |||
0.778801 | 0.778879 | 0.778802 | |||
0.697676 | 0.697756 | 0.697677 | |||
0.612626 | 0.612695 | 0.612627 | |||
0.527292 | 0.527337 | 0.527293 | |||
0.444858 | 0.444871 | 0.444858 | |||
0.367879 | 0.367856 | 0.367879 |
1 | 1 | 0 | 1 | 0 | |
1.01005 | 1.010078 | 1.01005 | |||
1.040811 | 1.040871 | 1.040811 | |||
1.094174 | 1.094299 | 1.094175 | |||
1.173511 | 1.173751 | 1.173513 | |||
1.284025 | 1.284458 | 1.284029 | |||
1.433329 | 1.434077 | 1.433337 | |||
1.632316 | 1.633578 | 1.632328 | |||
1.896481 | 1.898582 | 1.896501 | |||
2.247908 | 2.251381 | 2.247942 | |||
2.718282 | 2.724006 | 2.718338 |
CBSM |
||
CBSM |
||
[40] (n=4) | ||
[41] (j=3) | ||
[41] (j=4) |