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Article

Periodic Oscillatory Solutions for a Nonlinear Model with Multiple Delays

Department of Mathematics and Computer Science, Alabama State University, Montgomery, AL 36104, USA
Mathematics 2025, 13(14), 2275; https://doi.org/10.3390/math13142275
Submission received: 6 February 2025 / Revised: 30 June 2025 / Accepted: 2 July 2025 / Published: 15 July 2025

Abstract

For systems such as the van der Pol and van der Pol–Duffing oscillators, the study of their oscillation is currently a very active area of research. Many authors have used the bifurcation method to try to determine oscillatory behavior. But when the system involves n separate delays, the equations for bifurcation become quite complex and difficult to deal with. In this paper, the existence of periodic oscillatory behavior was studied for a system consisting of n coupled equations with multiple delays. The method begins by rewriting the second-order system of differential equations as a larger first-order system. Then, the nonlinear system of first-order equations is linearized by disregarding higher-degree terms that are locally small. The instability of the trivial solution to the linearized equations implies the instability of the nonlinear equations. Periodic behavior often occurs when the system is unstable and bounded, so this paper also studied the boundedness here. It follows from previous work on the subject that the conditions here did result in periodic oscillatory behavior, and this is illustrated in the graphs of computer simulations.

1. Introduction

Periodic oscillation is one of the key characteristics in a general class of nonlinear systems, and in coupled van der Pol-like systems in particular. Bifurcation can arise as a periodic solution. Therefore, many researchers have investigated various models of van der Pol or van der Pol-like oscillators by means of bifurcation or other methods. For example, Torres et al. [1] studied a triplet of mechanical oscillators equipped with a van der Pol term and having a Huygens coupling. These have a special coordinated motion. A transformation was used to reduce the system. Then, the system was analyzed using Poincare’s perturbation method. In [2], accurate analytical solutions were obtained for a system of three coupled van der Pol–Duffing oscillators. In [3], there was a system of four mixed-mode vibration types with a pitchfork bifurcation delay phenomenon. In [4], the oscillations of a hybrid van der Pol–Duffing–Rayleigh system were studied, both numerically and theoretically. In [5], bursting oscillations were analyzed in a complex coupled four-dimensional Mathieu–van der Pol oscillator. In [6], sufficient conditions were obtained for the exponential input-to-state stability of a coupled van der Pol system using graph theory and Kirchoff’s matrix-tree theorem. In [7], fold bifurcation and Hopf bifurcation were studied using the formal adjoin theory, the center manifold theorem, and the normal form method for a neutral differential–difference equation of the van der Pol type. In [8], Ghosh et al. studied zones of stability for a delayed Duffing–van der Pol system, which gave rise to a variety of synchronization channels. In [9], the original system was transformed into a three-dimensional system, and then all of the Darboux polynomials of a Mathieu–van der Pol–Duffing system were characterized and a complete system of rational first integrals was obtained. In [10], Sysoev proposed a method involving multivariate time series for the reconstruction of nonlinear coupling functions for all elements of ensembles of coupled van der Pol systems. In [11], Hoskoti et al. proposed a reduced-order method to study the oscillatory nature of wake dynamics caused by vortex shedding. This used a spring-mounted airfoil coupled with a van der Pol oscillator. In [12], a chaotic system of van der Pol oscillators coupled to linear oscillators was stabilized using adaptive control and synchronization. The authors of [13] investigated the stability and dynamic behavior of the simultaneous primary and super-harmonic resonance of a van der Pol oscillator. The authors of [14] investigated bifurcation structures in a van der Pol–Mathieu oscillator with external excitation. In [15], modulated motion and bifurcation were studied for two van der Pol oscillators that were nonlinearly coupled and parametrically excited. The authors of [16] studied the dynamic behavior of a van der Pol biorhythmic oscillator subjected to both colored noise and harmonic excitation. The authors of [17] conducted a systematic search of the parameter space for bi-rhythmic and tri-rhythmic families of van der Pol and Rayleigh oscillators and their higher-order variants using a numerical simulation. The authors of [18,19] studied the bifurcation characteristics of a van der Pol–Duffing oscillator subjected to white noise excitation and adaptive synchronization. They identified parameters for chaos to occur. In [20], the lateral oscillations of a pedestrian walking on a periodically moving floor were modeled by a modified van der Pol–Rayleigh oscillator. The authors of [21] studied voltage oscillations in a Bonhoeffer–van der Pol oscillator with a non-ideal capacitor. In 2011, Zhang et al. discussed the dynamic behavior of the following symmetric system [22]:
x 1 t + x 1 t ε 1 x 1 2 t x 1 t = k x 2 t τ x 1 t τ + k x 3 t τ x 1 t τ , x 2 t + x 2 t ε 1 x 2 2 t x 2 t = k x 1 t τ x 2 t τ + k x 3 t τ x 2 t τ , x 3 t + x 3 t ε 1 x 3 2 t x 3 t = k x 1 t τ x 3 t τ + k x 2 t τ x 3 t τ .
The dynamics of System (1) were carried out using a symmetric Hopf bifurcation result. Some important results about the spontaneous bifurcations of multiple branches of periodic solutions and their spatiotemporal patterns were obtained. Recently, Liu and Zhang extended Model (1) to four coupled van der Pol oscillators:
x 1 t = α p 2 x 1 2 t x 1 t x 1 t + a x 1 t τ + b x 2 t τ + c x 3 t τ + b x 4 t τ , x 2 t = α p 2 x 2 2 t x 2 t x 2 t + a x 2 t τ + b x 3 t τ + c x 4 t τ + b x 1 t τ , x 3 t = α p 2 x 3 2 t x 3 t x 3 t + a x 3 t τ + b x 4 t τ + c x 1 t τ + b x 2 t τ , x 4 t = α p 2 x 4 2 t x 4 t x 4 t + a x 4 t τ + b x 1 t τ + c x 2 t τ + b x 3 t τ .
where a , b ,   c , and τ > 0 are constants. By means of the symmetric Hopf bifurcation theory, the normal form of the system on the central manifold, the multiple periodic solutions of spatiotemporal patterns of the system were obtained and the bifurcating periodic solutions were also derived [23]. On the other hand, Nganso et al. considered the van der Pol oscillator with extended nonlinearity described by the following system:
x i t = μ 1 x i 2 t + α x i 4 t β x i 6 t   x i t + k 2 p k = i p i + p [ α ( x k t x i t ) + β x k t x i t ]
where i = 1 ,   2 ,   ,   n ,   k represents the strength of the coupling and α and β are the interaction parameters. A phenomenon of coupling-induced multi-stability was found in Model (3). A large limit cycle and a smaller quasi-periodic-like attractor were discussed [24]. Ji and Zhang discussed a van der Pol–Duffing oscillator:
x t μ x t + ω 2 x t μ x t τ ε x t τ + β x 2 t x t + α x 3 t k 1 x 3 t τ k 2 ( x ) 3 t τ k 3 x t τ x 2 t τ k 4 x t τ x t τ = 0
Hopf bifurcation and a quasi-periodic solution to Model (4) were investigated [25]. Motivated by the above models, in this paper, we studied the following n-coupled nonlinear differential system:
x 1 t = μ 1 1 x 1 2 t + α 1   x 1 4 t β 1   x 1 6 t x 1 t γ 1 x 1 t + k 1   x 1 3 t + a 11 x 1 t τ 1 + + a 1 n x n t τ n + k = 2 n p k 1 x k t τ k x 1 t τ 1 , x 2 t = μ 2 1 x 2 2 t + α 2   x 2 4 t β 2   x 2 6 t x 2 t γ 2 x 2 t + k 2   x 2 3 t + a 22 x 2 t τ 2 + + a 2 n x 1 t τ 1 + a 21 x 1 t τ 1 + k = 1 ,   k 2 n p k 2 x k t τ k x 2 t τ 2 , x 3 t = μ 3 1 x 3 2 t + α 3   x 3 4 t β 3   x 3 6 t x 3 t γ 3 x 3 t + k 3   x 3 3 t + a 33 x 3 t τ 3 + + a 3 n x 1 t τ 1 + a 31 x 1 t τ 1 + a 32 x 2 t τ 2 + k = 1 ,   i 3 n p k 3 x k t τ k x 3 t τ 3 ,   x n t = μ n 1 x n 2 t + α n   x n 4 t β n   x n 6 t x n t γ n x n t + k n   x n 3 t + a n n x n t τ n + a n 1 x 1 t τ 1 + + a n , n 1 x n 1 t τ n 1 + k = 1 n 1 p k n x k t τ k x n t τ n ,
where all the parameters are real numbers, 0 < μ i 1 , 0 < α i , β i , γ i ( i = 1 , 2 , , n ) , and the time delays are 0 < τ i i = 1 ,   2 ,   ,   n . We were concerned with the existence of periodic oscillatory solutions to Model (5). It is known that periodic solutions can arise from bifurcation. However, if time delays involve several different numbers, the bifurcation method is hard to carry out in Model (5) due to the complexity of the bifurcation equations. In the present paper, the method of mathematical analysis was used to deal with the question of oscillatory solutions to this model.

2. Preliminaries

System (5) can be expressed in the following equivalent form:
x 1 = x 2 , x 2 = μ 1 1 x 1 2 + α 1   x 1 4 β 1   x 1 6 x 2 γ 1 x 1 + k 1   x 1 3 + a 11 x 2 t τ 1 + a 12 x 4 t τ 2 + + a 1 n 1 x 2 n 2 t τ n 1 + a 1 n x 2 n t τ n + k = 2 n p 2 k 1,1 x 2 k 1 t τ k x 1 t τ 1 , x 3 = x 4 , x 4 = μ 2 1 x 3 2 + α 2   x 3 4 β 2   x 3 6 x 4 γ 2 x 3 + k 2   x 3 3 + a 22 x 4 t τ 2 + a 23 x 6 t τ 3 + + a 2 n x 2 n t τ n + a 21 x 2 t τ 1 + k = 1 ,   k 2 n p 2 k 1,3 x 2 k 1 t τ k x 3 t τ 2 , x 5 = x 6 , x 6 = μ 3 1 x 5 2 + α 3   x 5 4 β 3   x 5 6 x 6 γ 3 x 5 + k 3   x 5 3 + a 33 x 6 t τ 3 + a 34 x 8 t τ 4 + + a 3 n x 2 n t τ n + a 31 x 2 t τ 1 + a 32 x 4 t τ 2 + k = 1 ,   k 3 n p 2 k 1,5 x 2 k 1 t τ k x 5 t τ 3 , x 2 n 1 = x 2 n , x 2 n = μ n 1 x 2 n 1 2 + α n   x 2 n 1 4 β n   x 2 n 1 6 x 2 n γ n x 2 n 1 + k n   x 2 n 1 3 + a n n x 2 n t τ n + a n 1 x 2 t τ 1 + a n 2 x 4 t τ 2 + + a n , n 1 x 2 n 2 t τ n 1 + k = 1 n 1 p 2 k 1,2 n 1 x 2 k 1 t τ k x 2 n 1 t τ n ,
where x i = x i t , x i = x i t ( i = 1 , 2 , , 2 n ) . System (6) can be expressed as the following:
x 1 = x 2 , x 2 = γ 1 x 1 + μ 1 x 2 + a 11 x 2 t τ 1 + a 12 x 4 t τ 2 + + a 1 n 1 x 2 n 2 t τ n 1                   + a 1 n x 2 n t τ n + k = 2 n p 2 k 1,1 x 2 k 1 t τ k x 1 t τ 1 + k 1   x 1 3 + μ 1 x 1 2 + α 1   x 1 4 β 1   x 1 6 x 2 x 3 = x 4 , x 4 = γ 2 x 3 + μ 2 x 4 + a 22 x 4 t τ 2 + a 23 x 6 t τ 3 + + a 2 n x 2 n t τ n + a 21 x 2 t τ 1 + k = 1 ,   k 2 n p 2 k 1,3 x 2 k 1 t τ k x 3 t τ 2 + k 2   x 3 3 + μ 2 x 3 2 + α 2   x 3 4 β 2   x 3 6 x 4 x 5 = x 6 , x 6 = γ 3 x 5 + μ 3 x 6 + a 33 x 6 t τ 3 + a 34 x 8 t τ 4 + + a 3 n x 2 n t τ n + a 31 x 2 t τ 1 + a 32 x 4 t τ 2 + k = 1 ,   k 3 n p 2 k 1,5 x 2 k 1 t τ k x 5 t τ 3 + k 3   x 5 3 + μ 3 1 x 5 2 + α 3   x 5 4 β 3   x 5 6 x 6 x 2 n 1 = x 2 n , x 2 n = γ n x 2 n 1 + μ n x 2 n + a n n x 2 n t τ n + a n 1 x 2 t τ 1 + a n 2 x 4 t τ 2 + + a n , n 1 x 2 n 2 t τ n 1 + k = 1 n 1 p 2 k 1,2 n 1 x 2 k 1 t τ k x 2 n 1 t τ n + k n   x 2 n 1 3 + μ n x 2 n 1 2 + α n   x 2 n 1 4 β n   x 2 n 1 6 x 2 n
The matrix form of System (7) is as follows:
x t = A x t + B t τ + f ( x t ,
where x t = [ x 1 t , x 2 t , , x 2 n t ] T , x t τ = [ x 1 t τ 1 , x 2 t τ 1 , x 3 t τ 2 , , , x 2 n 1 t τ n , x 2 n t τ n ] T , A and B are both 2 n × 2 n matrices, and f ( x t ) is a 2 n -by-1 vector:
A = ( a i j ) 2 n × 2 n = 0 1 0 0 0 0 γ 1 μ 1 0 0 0 0 0 0 0 1 0 0 0 0 γ 2 μ 2 0 0 0 0 0 0 0 1 0 0 0 0 γ n μ n ,
B = ( b i j ) 2 n × 2 n = 0 0 0 0 0 0 b 21 b 22 b 23 b 24 b 2,2 n 0 0 0 0 0 0 b 41 b 42 b 43 b 44 b 4,2 n 0 0 0 0 0 0 b 2 n , 1 b 2 n , 2 b 2 n , 3 b 2 n , 4 b 2 n , 2 n ,
where b 21 = k = 2 n p 2 k 1,1 , b 22 = a 11 , b 22 = p 31 , b 24 = a 12 , , b 2,2 n 1 = p 2 n 1,1 , b 22 n = a 1 n , b 41 = p 13 , b 42 = a 21 , b 43 = k = 1 , k 2 n p 2 k 1,3 , b 44 = a 22 , , b 4,2 n 1 = p 2 n 1,3 , b 4,2 n = , , b 2 n , 1 = p 1,2 n 1 , b 2 n , 2 = a n 1 , b 2 n , 3 = p 3,2 n 1 , b 2 n , 4 = a n 2 , b 2 n , 2 n 1 = k = 1 n 1 p 2 k 1,2 n 1 , b 2 n 2 n = a n n , a n d   f x t = 0 ,   k 1   x 1 3 + μ 1 x 1 2 + α 1   x 1 4 β 1   x 1 6 x 2 ,     0 ,   k n   x 2 n 1 3 + μ n x 2 n 1 2 + α n   x 2 n 1 4 β n   x 2 n 1 6 x 2 n T . The linearized System (8) is as follows:
x t = A x t + B t τ .
Lemma 1. 
If matrix   S = A + B   is a nonsingular matrix for selected parameters, then there exists a unique equilibrium point for System (7) (or (8)).
Proof of Lemma 1. 
Assume that x * = [ x 1 * ,   x 2 * , , x 2 n * ] T is an equilibrium point of System (7); then, we have the following algebraic equations:
A x * + B x * + f x * = 0
Since matrix S = A + B , Equation (10) can be written as
S x * = f x *
Note that f 0 = 0 . So, there exists a trivial solution to (11). Since S = A + B is a nonsingular matrix, according to Cramer’s rule of linear algebra, Equation (11) has a unique solution, implying that System (7) has a unique trivial equilibrium. The proof is completed. □
Lemma 2. 
All solutions to System (6) (or (7)) are bounded, assuming that β i > 0   i = 1 ,   2 ,   ,   n .
Proof of Lemma 2. 
To prove the boundedness of the solutions in System (6), we constructed a Lyapunov function V t = i = 1 2 n 1 2 x i 2 ( t ) . By calculating the derivative of V t through System (6), we have
V t | ( 6 ) = i = 1 2 n x i t x i t = i = 1 n β i x 2 i 1 6 t x 2 i 2 t + i = 1 n α i x 2 i 1 4 t x 2 i 2 t i = 1 n μ i x 2 i 1 2 t x 2 i 2 t + i = 1 n k i x 2 i 1 3 t x 2 i t + i = 1 n μ i x 2 i 2 t
Note that β i i = 1 , 2 , , n are positive constants. Obviously, when x i + ( 1 i 2 n ) , x 2 i 1 6 x 2 i 2 are higher-order infinity than x 2 i 1 4 x 2 i 2 , x 2 i 1 2 x 2 i 2 i = 1 , 2 , , n , and so on. Therefore, there exists a suitably large K > 0 such that V t | ( 6 ) < 0 , as x i > K   i = 1 ,   2 ,   ,   2 n . This means that all solutions to System (6) (or (7)) are bounded. □

3. The Existence of Oscillatory Solutions

Theorem 1. 
Assume that System (7) (or (8)) has the unique trivial equilibrium point for selected parameter values. Let α 1 ,   α 2 ,   ,   α 2 n   and 0, β 1 ,   0 ,   β 2 ,     ,   0 ,   β n  be characteristic values of matrix A   and matrix B , respectively. Assume that Re( α 2 i 1 ) > 0 ( i = 1 ,   2 ,   ,   n ), or there exists a characteristic value, say   α 2 j , and Re( α 2 j ) > 0 with Re( α 2 j ) > | R e β j | + | I m   β j | ; then, the unique trivial solution to System (7) is unstable, implying that there exists an oscillatory solution in System (7).
Proof of Theorem 1.
Obviously, if the trivial solution to System (9) is unstable, then the trivial solution to System (7) (or (8)) is also unstable. Therefore, to discuss the instability of the trivial solution to System (7), we only need to deal with the instability of the trivial solution to System (9). The characteristic equation associated with System (9) is the following:
det λ   I i j A B e λ τ = 0
where I i j is the identity matrix of 2 n by 2 n . Noting that 0, β 1 ,   0 ,   β 2 ,     ,   0 ,   β n are characteristic values of matrix B , from (13), we have
λ α 2 i 1 = 0 , λ α 2 i β i   e λ τ i = 0 ,   i = 1,2 , ,   n .      
Thus, we are led to an investigation of the nature of the roots for some k ,   k { 1 ,   2 ,   ,   n }:
λ α 2 k 1 = 0 ,
or
λ α 2 k β k   e λ τ k = 0
For Equation (15), if Re( α 2 k 1 ) > 0, this implies that there is a positive real part characteristic value. So, the trivial solution to System (9) is unstable. Equation (16) is a transcendental equation for which it is hard to find all the solutions. However, we showed that the trivial solution to System (9) is unstable under the assumption of Theorem 1. Let λ =   λ 1 + i λ 2 ,     α 2 k = α 2 k , 1 + i α 2 k , 2   ,   β k = β k , 1 + i β k , 2 , where   λ 1 = R e λ ,   λ 2 = I m λ , α 2 k , 1 = R e   α 2 k , α 2 k , 2 = I m   α 2 k .     β k , 1 = R e   β k ,     β k , 2   = I m   β k , respectively. By separating the real part and imaginary part of Equation (16), we obtain the following:
  λ 1 α 2 k , 1 β k , 1   e   λ 1 τ k cos   ( λ 2 τ k ) + β k , 2   e   λ 1 τ k sin   ( λ 2 τ k ) = 0                          
  λ 2 α 2 k , 2 β k , 2   e   λ 1 τ k cos   ( λ 2 τ k ) β k , 1   e   λ 1 τ k sin   ( λ 2 τ k ) = 0                          
From the assumptions, there exists one     α j , and Re( α j ) > 0 with R e ( α j ) > | R e β j | + | I m   β j | ; we showed that Equation (17) has a positive real part root. Let
ϕ     λ 1 =   λ 1 α 2 j , 1 β j , 1   e   λ 1 τ j cos   ( λ 2 τ j ) + β j , 2   e   λ 1 τ j sin   ( λ 2 τ j )                          
Obviously, ϕ     λ 1   is a continuous function of   λ 1 . Noting that α 2 j , 1 > | β j , 1 | + β j , 2 ,     then ϕ   0 = α 2 j , 1 β j , 1 cos   ( λ 2 τ j ) + β j , 2   sin   ( λ 2 τ j )     α 2 j , 1 + β j , 1 + β j , 2 < 0 .                     Since e   λ 1 τ k 0 as   λ 1 + ,     there exists a suitably large   λ 1 , say λ 1 * , such that ϕ   λ 1 * = λ 1 * α 2 j , 1 β j , 1   e λ 1 * τ j cos   ( λ 2 τ j ) + β j , 2   e λ 1 * τ j sin   ( λ 2 τ j ) > 0 .                          
According to the intermediate value theorem, there exists a   λ 1 , say   λ 10 (0, λ 1 * ), such that ϕ     λ 10 = 0 ,   implying that there is a positive real part characteristic value of Equation (17). This means that the trivial solution to System (9) is unstable. Note that f ( x t ) of System (8) is a higher-order infinitesimal as   x i 0   i = 1,2 , ,   2 n . Therefore, the instability of the trivial solution to System (9) implies the instability of the trivial solution to nonlinear System (8). This suggests that the unique trivial equilibrium point of System (7) is unstable. This instability of the unique trivial equilibrium point, together with the boundedness of the solutions, will force System (7) (or (8)) to generate an oscillatory solution [26,27].
Now we adopt the following norms of the vector and matrix [28]:
x = i = 1 2 n   x i ,       B = max 1 j 2 n i = 1 2 n     b i j , and   let   s = m a x 1 i n γ i ,   1 + μ i .
Note that μ i > 0 ; thus,   s > 0 and we have the following:
Theorem 2. 
Assume that the conditions of Lemma 1 and Lemma 2 hold. Determine if the following inequality is satisfied:
7 s   B τ * 2 > 4   e s τ * ,
where   τ * = min τ 1 , τ 2 ,   ,     τ n .  If so, then the trivial solution to System (9) is unstable, implying that System (7) (or (8)) has an oscillatory solution.
Proof of Theorem 2. 
To prove the instability of the trivial solution to System (9), let y t = i = 1 2 n x i t . Therefore, y t > 0 and
y t s   y t + B   y ( t τ )
Specifically, consider a scalar equation:
z t = s   z t + B   z ( t τ )
According to the comparison theory of differential equations, we have y t z t . If the trivial solution to Equation (22) is unstable, then the trivial solution to (21) is still unstable. The characteristic equation associated with Equation (22) is given by
λ = s + B e λ τ
If the trivial solution to Equation (22) is stable, then Equation (23) must have a real negative root, say λ * , and from (23), we have
| λ * | > B e | λ * τ | s B e λ * τ * s
One can prove that the inequality e x 7 4 x 2 ( x > 0 ) holds. So, we have
1 B e λ * τ * λ * + s = B   τ * e λ * + s τ * e s τ * λ * + s τ * 7 B   τ * 2 λ * + s 4 e s τ * > 7 s B   τ * 2 4 e s τ *
A contradiction with Inequality (20) implies that the trivial solution to Equation (22) is unstable. This suggests that the trivial solution to Equation (21) is unstable, implying that the trivial solution to System (8) is unstable. Similar to Theorem 1, System (7) (or (8)) generates an oscillatory solution. The proof is completed. □

4. Simulation Result

Firstly, consider n = 5 in System (6) as the following:
x 1 = x 2 , x 2 = μ 1 1 x 1 2 + α 1   x 1 4 β 1   x 1 6 x 2 γ 1 x 1 + k 1   x 1 3 + a 11 x 2 t τ 1 + + a 15 x 10 t τ 5 + k = 2 5 p 2 k 1,1 x 2 k 1 t τ k x 1 t τ 1 , x 3 = x 4 , x 4 = μ 2 1 x 3 2 + α 2   x 3 4 β 2   x 3 6 x 4 γ 2 x 3 + k 2   x 3 3 + a 22 x 4 t τ 2 + a 23 x 6 t τ 3 + a 24 x 8 t τ 4 + + a 21 x 2 t τ 1 + k = 1 ,   k 2 5 p 2 k 1,3 x 2 k 1 t τ k x 3 t τ 2 , x 9 = x 10 , x 10 = μ 5 1 x 9 2 + α 5   x 9 4 β 5   x 9 6 x 10 γ 5 x 9 + k 5   x 9 3 + a 55 x 10 t τ 5 + a 51 x 2 t τ 1 + a 52 x 4 t τ 2 + + a 54 x 8 t τ 4 + k = 1 4 p 2 k 1,9 x 2 k 1 t τ k x 9 t τ 5 ,
The parameter values are shown in Table 1.
Then, the characteristic values of matrices A and B in System (26) are   0.0021 ± 0.9487 i ,   0.0022   ± 0.9747 i ,   0.0022 ± 0.9592 i , 0.0023   ± 0.9899 i , 0.0024 ± 0.9798 i , and 0.0015 ,   0.0446, 1.4635, 0.5417   ± 1.2873 i , 0, 0, 0, 0, 0, respectively. The time delays are selected as τ 1 = 1.15, τ 2 = 1 .16, τ 3 = 1.25 ,     τ 4 = 1.18 ,     τ 5 = 1.12 ,   and τ 1 = 1.65 ,     τ 2 = 1.66 ,     τ 3 = 1.75 ,     τ 4 = 1.68 ,     τ 5 = 1.62 , respectively. All the characteristic values of matrix A are complex numbers, and the real parts are greater than zero. Matrix B has a characteristic value of zero; thus the conditions of Theorem 1 are satisfied. There exists an oscillatory solution to System (26) (see Figure 1 and Figure 2). From Figure 1 and Figure 2, the curves of x 1   ( t ) , x 3   ( t ) , x 5   ( t ) , x 7   ( t ) , and x 9   ( t ) are smooth and the amplitude of x 1   ( t ) is only 4.0743. However, the curves of x 2   ( t ) , x 4   ( t ) , x 6   ( t ) , x 8   ( t ) , and x 10   ( t ) are jagged due to the higher order of variables in their equations. The amplitude of curve x 2   ( t ) is 14.1072. The oscillation frequency slows down as the time delay increases.
Then, consider n = 6 in System (6) as the following:
x 1 = x 2 , x 2 = μ 1 1 x 1 2 + α 1   x 1 4 β 1   x 1 6 x 2 γ 1 x 1 + k 1   x 1 3 + a 11 x 2 t τ 1 + + a 16 x 12 t τ 6 + k = 2 6 p 2 k 1,1 x 2 k 1 t τ k x 1 t τ 1 , x 3 = x 4 , x 4 = μ 2 1 x 3 2 + α 2   x 3 4 β 2   x 3 6 x 4 γ 2 x 3 + k 2   x 3 3 + a 22 x 4 t τ 2 + a 23 x 6 t τ 3 + a 24 x 8 t τ 4 + + a 21 x 2 t τ 1 + k = 1 ,   k 2 6 p 2 k 1,3 x 2 k 1 t τ k x 3 t τ 2 , x 11 = x 12 , x 12 = μ 6 1 x 11 2 + α 6   x 11 4 β 6   x 11 6 x 12 γ 6 x 11 + k 6   x 11 3 + a 66 x 12 t τ 6 + a 61 x 2 t τ 1 + a 62 x 4 t τ 2 + + a 65 x 10 t τ 5 + k = 1 5 p 2 k 1,11 x 2 k 1 t τ k x 11 t τ 5 ,
The parameters are shown in Table 2.
It is easy to see that s = 1.0148 and B = 4.74 in System (27). The time delays are selected as τ 1 = 0.75, τ 2 = 0 .78, τ 3 = 0.74 ,   τ 4 = 0.72 ,   τ 5 = 0.73 ,   τ 6 = 0.77 , and τ 1 = 1.05 , τ 2 = 1.08 ,   τ 3 = 1.04 ,   τ 4 = 1.02 ,   τ 5 = 1.03 , τ 6 = 1.07 , respectively. Then, τ * = 0.72 , and τ * = 1.02 . Thus, 7 s B τ * 2 = 7 × 1.0148 × 4.74 × 0.72 × 0.72 = 17.4551 > 8.3060 = 4 e s τ * and B τ * 2 = 7 × 1.0148 × 4.74 × 1.02 × 1.02 = 35.0314 > 11.2616 = 4 e s τ * . The conditions of Theorem 2 are satisfied. There exists an oscillatory solution to System (27) (see Figure 3 and Figure 4). From Figure 3 and Figure 4, the curves for odd subscripts are even and almost the same shapes, and the amplitude of x 1 ( t ) is 2.4018. The curves for even subscripts are steep and uneven, and the amplitude of x 2 ( t ) is 10.1625. The amplitude of the less-even curves is greater than that of the smooth curves. When the time delays increase, the oscillation frequencies decrease slightly.
Then, consider n = 7 in System (6) as the following:
x 1 = x 2 , x 2 = μ 1 1 x 1 2 + α 1   x 1 4 β 1   x 1 6 x 2 γ 1 x 1 + k 1   x 1 3 + a 11 x 2 t τ 1 + + a 17 x 14 t τ 7 + k = 2 7 p 2 k 1,1 x 2 k 1 t τ k x 1 t τ 1 , x 3 = x 4 , x 4 = μ 2 1 x 3 2 + α 2   x 3 4 β 2   x 3 6 x 4 γ 2 x 3 + k 2   x 3 3 + a 22 x 4 t τ 2 + a 23 x 6 t τ 3 + + a 27 x 14 t τ 7 + a 21 x 2 t τ 1 + k = 1 ,   k 2 7 p 2 k 1,3 x 2 k 1 t τ k x 3 t τ 2 , x 13 = x 14 , x 14 = μ 7 1 x 13 2 + α 7   x 13 4 β 7   x 13 6 x 14 γ 7 x 13 + k 7   x 13 3 + a 77 x 14 t τ 7 + a 71 x 2 t τ 1 + a 72 x 4 t τ 2 + + a 76 x 12 t τ 6 + k = 1 6 p 2 k 1,13 x 2 k 1 t τ k x 13 t τ 7 ,
The parameters are shown in Table 3.
The characteristic values of matrices A and B in System (28) are   0.0140 ± 1.7748 i ,     0.0140 ± 1.7719 i ,       0.0140 ± 1.7832 i ,       0.0145 ± 1.7776 i ,       0.0145 ± 1.7725 i ,   0.0145 ± 1.7714 i ,     0.1450 ± 1.7604 i , and   0.0016 , 0.1385 , 0.2426 ,   0.2438 ± 0.6337 i ,   1.3726 ± 0.7414 i ,       0 ,     0 ,     0 ,     0 ,     0 ,     0 ,     0 , respectively. The time delays are selected as τ 1 = 0.75, τ 2 = 0 .78, τ 3 = 0.80 ,     τ 4 = 0.76 ,     τ 5 = 0.74 ,     τ 6 = 0.77 ,     τ 7 = 0.72 ,   and τ 1 = 0.85 ,   τ 2 = 0.88 , τ 3 = 0.90 ,   τ 4 = 0.86 ,   τ 5 = 0.84 ,   τ 6 = 0.87 ,   τ 7 = 0.82 , respectively. It is easy to see that the conditions of Theorem 1 are satisfied. There exists an oscillatory solution to System (28) (see Figure 5 and Figure 6). The curves for odd subscripts are even and the curves for even subscripts are uneven. In Figure 5, the amplitude of   x 1 ( t ) is just 3.3591, but that for x 8 ( t ) is 12.6238. Figure 5 and Figure 6 indicate that the time delay affects the oscillation frequency. A change in the time delays will cause a change in the oscillatory frequency.
Finally, we considered n = 8 in System (6) as the following:
x 1 = x 2 , x 2 = μ 1 1 x 1 2 + α 1   x 1 4 β 1   x 1 6 x 2 γ 1 x 1 + k 1   x 1 3 + a 11 x 2 t τ 1 + + a 18 x 16 t τ 8 + k = 2 8 p 2 k 1,1 x 2 k 1 t τ k x 1 t τ 1 , x 3 = x 4 , x 4 = μ 2 1 x 3 2 + α 2   x 3 4 β 2   x 3 6 x 4 γ 2 x 3 + k 2   x 3 3 + a 22 x 4 t τ 2 + a 23 x 6 t τ 3 + + a 28 x 16 t τ 8 + a 21 x 2 t τ 1 + k = 1 ,   k 2 8 p 2 k 1,3 x 2 k 1 t τ k x 3 t τ 2 , x 15 = x 16 , x 16 = μ 8 1 x 15 2 + α 8   x 15 4 β 8   x 15 6 x 16 γ 8 x 15 + k 8   x 15 3 + a 88 x 16 t τ 8 + a 81 x 2 t τ 1 + a 82 x 4 t τ 2 + + a 87 x 14 t τ 7 + k = 1 7 p 2 k 1,15 x 2 k 1 t τ k x 15 t τ 8 ,
From Table 4, s = 1.0019 and B = 7.65. The time delays are selected as τ 1 = 0.38, τ 2 = 0 .40, τ 3 = 0.42 ,   τ 4 = 0.43 ,   τ 5 = 0.36 ,   τ 6 = 0.41 ,   τ 8 = 0.39, Thus, τ * = 0.35 ,   7 s B τ * 2 = 7 × 1.0018 × 7.65 × 0.35 × 0.35 = 6.5723 > 5.5801 = 4 e s τ * . The conditions of Theorem 2 are satisfied. There exists an oscillatory solution to System (29) (see Figure 7 and Figure 8). Figure 7 and Figure 8 indicate that the values of γ i   i = 1,2 , , 8 affect the oscillation frequency. The parameters in the two figures are almost the same. In Figure 8, only the parameters γ i are less than the values of γ i   i = 1,2 , , 8 in Figure 7. The oscillation frequencies are different from each other.
The values of γ i   were   selected   as   2.55 , 2.56 , 2.52 , 2.58 , 2.50 , 2.54 , 2.57 ,   and   2.60 .
The values of γ i   were   selected   as   1.55 , 1.56 , 1.52 , 1.58 , 1.50 , 1.54 , 1.57 ,   and   1.60 .

5. Discussion

The present criteria only determine the existence of oscillatory solutions. They cannot provide the bifurcation values about the delays. It is pointed out that it is difficult to deal with the present models using the bifurcation method. Even if for n = 5 , the bifurcation equation will be the following:
p 0 10 λ + i = 1 5 p i 9 λ e λ τ i + i j p i 8 λ e λ ( τ i + τ j ) + + p 0 e λ τ 1 + + τ 5 = 0 ,
where p 0 10 λ is a ten-order polynomial,   p i 9 λ   ( i = 1,2 , ,   5 ) are nine-order polynomials about λ , and p 0 is a constant. If τ i   ( i = 1,2 , ,   5 )   are different real numbers, then λ τ i ( i = 1,2 , ,   5 ) are different variables. Equation (30) is a transcendental equation with five different variables. Theoretically, one can use Ruan’s method to find the bifurcation values [29]. However, finding the bifurcating values from Equation (30) is not easy work.

6. Conclusions

Gap differential equations of types related to the van der Pol and van der Pol–Duffing equations are difficult to study directly from the bifurcation conditions when the system involves many gaps. In this paper, it was shown that, alternatively, a study of these systems can be effective with a method of reduction to first-order, linearization, and the determination of the instability of the trivial solution, together with boundedness. This is shown by the periodic appearance of the graphs for simulations with randomly chosen parameters. Two theorems are proved in this paper that provide sufficient conditions.

Funding

This research received no external funding.

Data Availability Statement

The original contributions presented in this study are included in the article. Further inquiries can be directed to the author.

Conflicts of Interest

The author declares no conflicts of interest.

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Figure 1. Oscillations of the solutions; delays: 1.15, 1.16, 1.25, 1.18, and 1.12.
Figure 1. Oscillations of the solutions; delays: 1.15, 1.16, 1.25, 1.18, and 1.12.
Mathematics 13 02275 g001
Figure 2. Oscillations of the solutions; delays: 1.65, 1.66, 1.75, 1.68, and 1.62.
Figure 2. Oscillations of the solutions; delays: 1.65, 1.66, 1.75, 1.68, and 1.62.
Mathematics 13 02275 g002
Figure 3. Oscillations of the solutions; delays: 0.75, 0.78, 0.74, 0.72, 0.73, and 0.77.
Figure 3. Oscillations of the solutions; delays: 0.75, 0.78, 0.74, 0.72, 0.73, and 0.77.
Mathematics 13 02275 g003
Figure 4. Oscillations of the solutions; delays: 1.05, 1.08, 1.04, 1.02, 1.03, and 1.07.
Figure 4. Oscillations of the solutions; delays: 1.05, 1.08, 1.04, 1.02, 1.03, and 1.07.
Mathematics 13 02275 g004
Figure 5. Oscillations of the solutions; delays: 0.75, 0.78, 0.80, 0.76, 0.74, 0.77, and 0.72.
Figure 5. Oscillations of the solutions; delays: 0.75, 0.78, 0.80, 0.76, 0.74, 0.77, and 0.72.
Mathematics 13 02275 g005
Figure 6. Oscillations of the solutions; delays: 0.85, 0.88, 0.90, 0.86, 0.84, 0.87, and 0.82.
Figure 6. Oscillations of the solutions; delays: 0.85, 0.88, 0.90, 0.86, 0.84, 0.87, and 0.82.
Mathematics 13 02275 g006
Figure 7. Oscillations of the solutions; delays: 0.38, 0.40, 0.42, 0.43, 0.36, 0.36, 0.41, and 0.39.
Figure 7. Oscillations of the solutions; delays: 0.38, 0.40, 0.42, 0.43, 0.36, 0.36, 0.41, and 0.39.
Mathematics 13 02275 g007
Figure 8. Oscillations of the solutions; delays: 0.38, 0.40, 0.42, 0.43, 0.36, 0.36, 0.41, and 0.39.
Figure 8. Oscillations of the solutions; delays: 0.38, 0.40, 0.42, 0.43, 0.36, 0.36, 0.41, and 0.39.
Mathematics 13 02275 g008
Table 1. The parameter values in System (26).
Table 1. The parameter values in System (26).
μ1μ2μ3μ4μ5α1α2α3α4α5
0.00450.00480.00440.00460.00420.750.740.720.780.82
β1β2β3β4β5γ1γ2γ3γ4γ5
0.650.680.620.640.660.950.960.920.980.90
k1k2k3k4k5a11a12a13a14a15
0.00150.00180.00120.00160.00140.82−0.880.85−0.860.84
a21a22a23a24a25a31a32a33a34a35
1.161.15−1.101.18−1.140.84−0.870.86−0.850.84
a41a42a43a44a45a51a52a53a54a55
0.92−0.980.94−0.960.950.750.720.78−0.760.71
p31p51p71p91 p13p53p73p93
0.76−0.780.720.90 0.35−0.320.340.30
p15p35p75p95 p17p37p57p97
0.24−0.250.280.32 0.70−0.520.480.46
p19p39p59p79
0.52−0.450.480.42
Table 2. The parameter values in System (27).
Table 2. The parameter values in System (27).
μ1μ2μ3μ4μ5μ6α1α2α3α4α5α6
0.01450.01480.01440.01460.01420.01430.250.240.220.280.260.27
β1β2β3β4β5β6γ1γ2γ3γ4γ5γ6
1.551.681.621.641.661.602.952.962.922.982.902.93
k1k2k3k4k5k6a11a12a13a14a15a16
0.150.180.120.160.140.170.12−0.380.15−0.360.140.13
a21a22a23a24a25a26a31a32a33a34a35a36
0.160.15−0.100.18−0.140.130.42−0.280.46−0.450.440.42
a41a42a43a44a45a46a51a52a53a54a55a56
0.52−0.580.54−0.660.45−0.660.450.420.48−0.360.460.40
a61a62a63a64a65a66p31p51p71p91p111
0.72−0.740.700.68−0.620.660.78−0.750.720.700.74
p13p53p73p93p113 p15p35p75p95p115
0.35−0.620.34−0.400.32 0.240.26−0.380.340.37
p17p37p57p97p117 p19p39p59p79p119
0.70−0.720.480.460.50 0.52−0.450.480.420.46
p111p311p511p711p911
0.62−0.780.680.64−0.70
Table 3. The parameter values in System (28).
Table 3. The parameter values in System (28).
μ1μ2μ3μ4μ5μ6μ7
0.02840.02920.02950.02860.02880.02830.0281
α1α2α3α4α5α6α7
0.150.140.120.180.160.130.10
β1β2β3β4β5β6β7
0.650.680.620.640.660.600.65
γ1γ2γ3γ4γ5γ6γ7
3.153.163.123.183.103.143.17
k1k2k3k4k5k6k7
0.0150.0200.0120.0160.0180.0130.014
a11a12a13a14a15a16a17a21a22a23a24a25a26
0.34−0.460.45−0.260.420.33−0.370.360.35−0.390.38−0.340.35
a27a31a32a33a34a35a36a37a41a42a43a44a45
0.370.42−0.380.46−0.450.440.430.470.53−0.580.54−0.660.55
a46a47a51a52a53a54a55a56a57a61a62a63a64
−0.540.560.760.720.75−0.760.720.79−0.680.650.630.66−0.65
a65a66a67a71a72a73a74a75a76a77
0.640.57−0.680.650.610.68−0.620.670.690.63
p31p51p71p91p111p131p13p53p73p93p113p133
0.700.78−0.760.730.740.680.36−0.320.30−0.400.36−0.38
p15p35p75p95p115p135p17p37p57p97p117p137
0.26−0.52−0.460.430.410.440.72−0.640.630.650.640.53
p19p39p59p79p119p139p111p311p5,11p7,11p9,11p13,11
0.55−0.480.420.480.470.400.54−0.580.460.52−0.670.54
p1,13p3,13p5,13p7,13p9,13p11,13
0.470.580.360.45−0.540.41
Table 4. The parameter values in System (29).
Table 4. The parameter values in System (29).
μ1μ2μ3μ4μ5μ6μ7μ8
0.00150.00120.00130.00160.00180.00140.00190.0017
α1α2α3α4α5α6α7α8
0.550.540.520.580.560.530.600.62
β1β2β3β4β5β6β7β8
0.950.980.920.940.960.930.970.91
γ1γ2γ3γ4γ5γ6γ7γ8
2.552.562.522.582.502.542.572.60
k1k2k3k4k5k6k7k8
0.0060.0030.0070.0040.0080.0090.0040.005
a11a12a13a14a15a16a17a18a21a22a23a24a25
0.410.480.450.460.440.430.470.500.46−0.580.400.480.55
a26a27a28a31a32a33a34a35a36a37a38a41a42
−0.650.570.670.72−0.780.76−0.760.74−0.720.780.750.62−0.72
a43a44a45a46a47a48a51a52a53a54a55a56a57
0.34−0.46−0.55−0.730.770.420.650.620.81−0.560.820.47−0.65
a58a61a62a63a64a65a66a67a68a71a72a73a74
0.540.550.520.58−0.540.610.57−0.860.630.450.420.48−0.46
a75a76a77a78a81a82a83a84a86a87a88
0.520.470.570.500.650.640.61−0.350.680.65−0.54
p31p51p71p91p111p131p151p13p53p73p93p113p133
0.76−0.780.820.800.810.750.710.450.320.41−0.54−0.540.46
p153p15p35p75p95p115p135p155p17p37p57p97p117
0.550.54−0.650.480.520.57−0.580.54−0.720.78−0.68−0.760.72
p137p157p19p39p59p79p119p139p159p11p311p511p711
−0.460.380.62−0.450.480.420.560.510.360.35−0.480.580.54
p911p1311p1511p1,13p3,13p5,13p7,13p9,13p11,13p15,13p1,15p3,15p5,15
−0.680.440.480.550.42−0.440.46−0.480.500.500.55−0.520.56
p7,15p9,15p11,15p13,15
0.54−0.440.480.40
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Feng, C. Periodic Oscillatory Solutions for a Nonlinear Model with Multiple Delays. Mathematics 2025, 13, 2275. https://doi.org/10.3390/math13142275

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Feng, Chunhua. 2025. "Periodic Oscillatory Solutions for a Nonlinear Model with Multiple Delays" Mathematics 13, no. 14: 2275. https://doi.org/10.3390/math13142275

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Feng, C. (2025). Periodic Oscillatory Solutions for a Nonlinear Model with Multiple Delays. Mathematics, 13(14), 2275. https://doi.org/10.3390/math13142275

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