CN106777738A - A kind of numerical computation method for variable mass dynamical system - Google Patents
A kind of numerical computation method for variable mass dynamical system Download PDFInfo
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- CN106777738A CN106777738A CN201611231387.7A CN201611231387A CN106777738A CN 106777738 A CN106777738 A CN 106777738A CN 201611231387 A CN201611231387 A CN 201611231387A CN 106777738 A CN106777738 A CN 106777738A
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Abstract
The invention discloses a kind of numerical computation method for variable mass dynamical system, comprise the following steps:Determine integral parameter γ, β (t) and step delta t, calculate integration variable, obtain the system mode of t, obtain t, the systematic parameter of t+ Δ ts, calculate the effective rigidity of t+ Δ ts, calculate the payload of t+ Δ ts, payload is the displacement of t+ Δ ts with the business of effective rigidity, using the system mode of t, the displacement of quality and t+ Δ ts, speed of the Mass Calculation system in t+ Δ ts, by the displacement of t+ Δ ts, the acceleration of speed and Mass Calculation system in t+ Δ ts, and then iterate to calculate, finally try to achieve all vibratory responses in the range of required time-histories.The present invention not only considers influence of the quality to system displacement, speed and acceleration, and in view of integral parameter and the influence factor of step-length, makes algorithm computational accuracy preferable.
Description
Technical field
The present invention relates to a kind of numerical computation method for variable mass dynamical system, belong to numerical analysis simulation technology neck
Domain.
Background technology
In recent years, due to the development of aeronautical and space technology and industrial technology, the research of variable mass dynamical system is increasingly received
To the attention of researcher, such as rocket, aircraft and vehicle bridge coupling vibration system.Variable mass dynamical system vibration characteristics is different from
Constant-quality dynamical system, its research is also long-standing, and early in 1897, Russia's scholar Mi Xie Bielskis were just proposed for grinding
Study carefully the dynamic (dynamical) close Bielski equation of having a rest of variable mass particle.
Single-degree-of-freedom variable mass dynamical system, as shown in figure 1, in Fig. 1 m (t), c, k represent respectively mass of system, damping and
Rigidity, quality m (t) is the function with time correlation;X and f represent system displacement and extraneous exciting force respectively.Variable mass dynamical system
Subordination is in nonlinear dynamic system, if direct solution kinetic equation is relatively difficult, cannot even solve sometimes, therefore researcher
Method frequently with numerical computations asks its vibratory response.Chinese invention patent " variable mass dynamic vibration absorber transient process emulation side
Method " (publication No.:CN 103851125A) disclose a kind of numerical computations for solving variable mass dynamic vibration absorber transient process
Method, the method takes into consideration only influence of the mass change to system speed and acceleration, but does not consider integral parameter
With the influence factor of step-length, its computational accuracy has much room for improvement.It is published in《Mechanics journal》Scientific paper on the 5th phase of volume 44
" the adaptive N ewmark methods cooperateed with Structure Dynamic Characteristics " is set up when variable mass dynamical system vibratory response is calculated
Vibration equation need to consider influence of the mass change to damping, and the Mathematical Modeling set up is more complicated.
The content of the invention
The technical problems to be solved by the invention are the defects for overcoming prior art, there is provided one kind is used for variable mass dynamical system
The vibration processes of variable mass dynamical system can be carried out simulation calculation by the numerical computation method of system.
In order to solve the above technical problems, the present invention provides a kind of numerical computation method for variable mass dynamical system, bag
Include following steps:
1) integral parameter γ, β (t) and step delta t are determined:
The integral parameter γ is set to:γ=1/2,
Integral parameter β (t) is defined as:
The step delta t meets:
Wherein,
K represents the rigidity of variable mass dynamical system, mtThe quality of variable mass dynamical system t is represented, c represents variable mass
The damping of dynamical system;
2) integration variable α is calculated0(t), α1(t), α2(t), α3(t), α4(t), α5(t);
3) the state x of variable mass dynamical system t is obtainedtWithWherein, xtRepresent variable mass dynamical system t position
Move,Represent variable mass dynamical system t speed;It is known for the variable mass dynamical system state that initial time t is 0
Amount, when dynamic response is solved, the displacement of known initial time and speed;For the state at t ≠ 0 moment, by the t-1 moment
Calculating obtain;
4) the variable mass power system parameter of t, t+ Δ t is obtained, including:The quality of t variable mass dynamical system
mt, the quality m of t+ Δ t variable mass dynamical systemst+Δt, the extraneous exciting force f of t variable mass dynamical systemt, during t+ Δ t
Carve the extraneous exciting force f of variable mass dynamical systemt+Δt, the damping c and rigidity k of variable mass dynamical system;
5) effective rigidity of t+ Δ ts is calculated
6) the effective extraneous exciting force of t+ Δ ts is calculated
7) displacement x of t+ Δ ts is solvedt+Δt;
8) speed of t+ Δ ts is solvedAnd acceleration
9) t=t+ Δs t is made;
10) repeat step 1) to the system response for 9), calculating subsequent time, finally try to achieve all in the range of required time-histories
Vibratory response.
Foregoing step 2) in integration variable computing formula it is as follows:
Foregoing step 5) effective rigidityComputing formula it is as follows:
Foregoing step 6) effectively extraneous exciting forceComputing formula it is as follows:
Wherein,Represent variable mass dynamical system t acceleration.
Foregoing step 7) t+ Δ ts displacement xt+ΔtComputing formula it is as follows:
Wherein,It is the effective rigidity of t+ Δ ts.
Foregoing step 8) t+ Δ ts speedAnd accelerationComputing formula it is as follows:
The beneficial effect that the present invention is reached:
(1) numerical computation method of the invention when variable mass dynamical system vibratory response is calculated, shake by the system for being used
Dynamic equation is not required to influence of the consideration mass change to damping, therefore, build variable mass dynamical system vibration equation and be easier.
(2) it is of the invention in calculating process, the not only influence in view of quality to system displacement, speed and acceleration, and
And in view of integral parameter and the influence factor of step-length, make algorithm computational accuracy preferable.
(3) numerical computation method applicability of the invention is wide, can be used for all of variable mass dynamical system.
Brief description of the drawings
Fig. 1 is variable mass dynamical system one degree of freedom modeling;
Fig. 2 is using numerical computation method of the invention and adaptive N ewmark algorithms, tradition Newmark algorithms gained
Result of calculation comparison diagram.
Specific embodiment
The invention will be further described below.Following examples are only used for clearly illustrating technical side of the invention
Case, and can not be limited the scope of the invention with this.
Numerical computation method for variable mass dynamical system of the invention, specifically includes following steps:
Step one, determines integral parameter γ, β (t) and step delta t:
Integral parameter γ is set to:γ=1/2,
Integral parameter β (t) is defined as:
Step delta t meets:
Wherein,
Wherein, in formula (3),
K represents the rigidity of variable mass dynamical system, mtThe quality of variable mass dynamical system t is represented, c represents variable mass
The damping of dynamical system.
Step 2, calculates integration variable α0(t), α1(t), α2(t), α3(t), α4(t), α5(t):
Step 3, obtains the state (x of variable mass dynamical system t (initial time t is 0)t、), xtRepresent variable mass
Dynamical system t displacement,Represent variable mass dynamical system t speed;It is known for the state that initial time t is 0
Amount, when dynamic response is solved, the displacement of known initial time and speed;For the state at t ≠ 0 moment, by the t-1 moment
Calculating obtain.
Step 4, obtains the variable mass power system parameter of t, t+ Δ t, including:T variable mass dynamical system
Quality mt, the quality m of t+ Δ t variable mass dynamical systemst+Δt, the extraneous exciting force f of t variable mass dynamical systemt, t+
The extraneous exciting force f of Δ t variable mass dynamical systemt+Δt, the damping c and rigidity k of variable mass dynamical system.
Step 5, calculates the effective rigidity of t+ Δ tsComputing formula is as follows:
Above-mentioned computing formula is to add rotten secondary element on the basis of Newmark algorithms and change integration variable to obtain
's.
Step 6, calculates the effective extraneous exciting force of t+ Δ tsComputing formula is as follows:
Wherein,Variable mass dynamical system t acceleration is represented,
Above-mentioned computing formula is to add rotten secondary element on the basis of Newmark algorithms and change integration variable to obtain
's.
Step 7, solves the displacement x of t+ Δ tst+Δt, computing formula is as follows:
Above-mentioned computing formula is to add rotten secondary element on the basis of Newmark algorithms and change integration variable to obtain
's.
Step 8, solves the speed of t+ Δ tsAnd accelerationComputing formula is as follows:
Above-mentioned computing formula is to add rotten secondary element on the basis of Newmark algorithms and change integration variable to obtain
's.
Step 9, makes t=t+ Δs t;
Step 10, repeats the above steps one to nine, calculates the system response of subsequent time, finally tries to achieve required time-histories scope
Interior all vibratory responses.
Embodiment
Below by proposed by the invention to verify with adaptive N ewmark algorithms and the contrast of tradition Newmark algorithms
Numerical computation method.Using numerical computation method of the present invention, the single-degree-of-freedom variable mass system model shown in Fig. 1 is imitated
It is true to calculate, mass of system m in Fig. 1t, rigidity k and damping c it is as shown in table 1.
The variable mass system parameter of table 1
From table 1 it follows that mass of system mtIt is the variable changed with time t, in initial time m0It is 1.Suffered by system
Extraneous exciting force ftIt is sin10t, initial displacement x0, speed0 is taken respectively.
Numerical computation method of the invention, adaptive N ewmark algorithms and tradition Newmark algorithm calculated results
As shown in Figure 2.Fig. 2 is variable mass system acceleration responsive when material calculation is 0.01s, it can be seen that of the invention
Numerical computation method acquired results are consistent with adaptive N ewmark algorithms, tradition Newmark algorithms, and in two algorithms gained
Between result, so as to illustrate numerical computation method of the invention for calculating the effective of variable mass dynamic vibration absorber vibratory response
Property.In Fig. 2,Inventive algorithm is represented, ----adaptive N ewmark algorithms are represented, --- -- represents tradition Newmark
Algorithm.
The above is only the preferred embodiment of the present invention, it is noted that for the ordinary skill people of the art
For member, on the premise of the technology of the present invention principle is not departed from, some improvement and deformation can also be made, these improve and deform
Also should be regarded as protection scope of the present invention.
Claims (6)
1. a kind of numerical computation method for variable mass dynamical system, it is characterised in that comprise the following steps:
1) integral parameter γ, β (t) and step delta t are determined:
The integral parameter γ is set to:γ=1/2,
Integral parameter β (t) is defined as:
The step delta t meets:
Wherein,
K represents the rigidity of variable mass dynamical system, mtThe quality of variable mass dynamical system t is represented, c represents variable mass power
The damping of system;
2) integration variable α is calculated0(t), α1(t), α2(t), α3(t), α4(t), α5(t);
3) the state x of variable mass dynamical system t is obtainedtWithWherein, xtVariable mass dynamical system t displacement is represented,
Represent variable mass dynamical system t speed;It is known quantity for the variable mass dynamical system state that initial time t is 0, is asking
During solution dynamic response, the displacement of known initial time and speed;For the state at t ≠ 0 moment, by the calculating at t-1 moment
Obtain;
4) the variable mass power system parameter of t, t+ Δ t is obtained, including:The quality m of t variable mass dynamical systemt, t+
The quality m of Δ t variable mass dynamical systemt+Δt, the extraneous exciting force f of t variable mass dynamical systemt, the change of t+ Δs t
The extraneous exciting force f of quality power systemt+Δt, the damping c and rigidity k of variable mass dynamical system;
5) effective rigidity of t+ Δ ts is calculated
6) the effective extraneous exciting force of t+ Δ ts is calculated
7) displacement x of t+ Δ ts is solvedt+Δt;
8) speed of t+ Δ ts is solvedAnd acceleration
9) t=t+ Δs t is made;
10) repeat step 1) to the system response for 9), calculating subsequent time, finally try to achieve all vibrations in the range of required time-histories
Response.
2. a kind of numerical computation method for variable mass dynamical system according to claim 1, it is characterised in that described
Step 2) in integration variable computing formula it is as follows:
3. a kind of numerical computation method for variable mass dynamical system according to claim 1, it is characterised in that described
Step 5) effective rigidityComputing formula it is as follows:
4. a kind of numerical computation method for variable mass dynamical system according to claim 1, it is characterised in that described
Step 6) effectively extraneous exciting forceComputing formula it is as follows:
Wherein,Represent variable mass dynamical system t acceleration.
5. a kind of numerical computation method for variable mass dynamical system according to claim 4, it is characterised in that described
Step 7) t+ Δ ts displacement xt+ΔtComputing formula it is as follows:
Wherein,It is the effective rigidity of t+ Δ ts.
6. a kind of numerical computation method for variable mass dynamical system according to claim 1, it is characterised in that described
Step 8) t+ Δ ts speedAnd accelerationComputing formula it is as follows:
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Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050155431A1 (en) * | 2004-01-19 | 2005-07-21 | Mayumi Fukuyama | Vibration test system and method for structures |
CN103423368A (en) * | 2013-07-18 | 2013-12-04 | 长安大学 | Variable mass dynamic vibration absorber control method |
CN103851125A (en) * | 2014-02-12 | 2014-06-11 | 长安大学 | Variable-mass power vibration absorber transient process simulation method |
-
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- 2016-12-28 CN CN201611231387.7A patent/CN106777738A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20050155431A1 (en) * | 2004-01-19 | 2005-07-21 | Mayumi Fukuyama | Vibration test system and method for structures |
CN103423368A (en) * | 2013-07-18 | 2013-12-04 | 长安大学 | Variable mass dynamic vibration absorber control method |
CN103851125A (en) * | 2014-02-12 | 2014-06-11 | 长安大学 | Variable-mass power vibration absorber transient process simulation method |
Non-Patent Citations (3)
Title |
---|
王宇楠 等: "变质量梁的自适应Newmark法", 《北京航空航天大学学报》 * |
赵艳青: "基于Newmark算法的变质量动力吸振器仿真方法研究", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 * |
邢誉峰 等: "与结构动特性协同的自适应Newmark方法", 《力学学报》 * |
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