CN107704714B - Method and system for processing finite element simulation stress value and test stress value - Google Patents

Method and system for processing finite element simulation stress value and test stress value Download PDF

Info

Publication number
CN107704714B
CN107704714B CN201711075619.9A CN201711075619A CN107704714B CN 107704714 B CN107704714 B CN 107704714B CN 201711075619 A CN201711075619 A CN 201711075619A CN 107704714 B CN107704714 B CN 107704714B
Authority
CN
China
Prior art keywords
stress value
test
value
stress
calculating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
CN201711075619.9A
Other languages
Chinese (zh)
Other versions
CN107704714A (en
Inventor
刘亚妮
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CRRC Zhuzhou Locomotive Co Ltd
Original Assignee
CRRC Zhuzhou Locomotive Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by CRRC Zhuzhou Locomotive Co Ltd filed Critical CRRC Zhuzhou Locomotive Co Ltd
Priority to CN201711075619.9A priority Critical patent/CN107704714B/en
Publication of CN107704714A publication Critical patent/CN107704714A/en
Application granted granted Critical
Publication of CN107704714B publication Critical patent/CN107704714B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation
    • G06F30/23Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]

Abstract

The invention discloses a method and a system for processing finite element simulation stress values and test stress values, which comprises the following steps: calculating the absolute error between the simulated stress value and the test stress value; calculating the utilization rate of the material, the relative error between the simulated stress value and the test stress value, and calculating the matching rate of the simulated stress value and the test stress value by using the relative error; and drawing by taking the utilization rate of the material as an X axis and the matching rate as a Y axis to obtain the relationship among the simulated stress value, the test stress value and the allowable stress. The invention can observe the relation among the test value, the simulation value and the allowable stress visually, and fills the blank of processing data at present; the method intuitively, accurately and reasonably expresses the relation between the test result and the simulation result, is associated with the actual application scene, is objective and is suitable for engineering application.

Description

Method and system for processing finite element simulation stress value and test stress value
Technical Field
The invention relates to the field of mechanical design, in particular to a method and a system for processing finite element simulation stress values and test stress values.
Background
Finite element analysis enables engineers to pre-identify potential problems prior to product manufacture or construction, shorten design and analysis cycle times, add design functionality, reduce design costs, and simulate various test scenarios, reducing test time and expense. It is therefore a very common approach in the field of mechanical design to determine design strength using finite element analysis.
In the stages of design completion and prototype manufacturing completion, necessary static strength tests are performed in order to verify the correctness of the simulation or to meet the standard. When the static strength test is finished, the test stress value and the simulation stress value error need to be compared, but the current general comparison method judges the relation between the test value and the simulation value by calculating the relative error and the absolute error between the test value and the simulation value, and the two errors can not intuitively, accurately and reasonably express the relation between the test result and the simulation result and can not be associated with the actual application scene, namely can not be associated with the allowable stress value of the material under the application scene.
Disclosure of Invention
The technical problem to be solved by the invention is to provide a method and a system for processing finite element simulation stress values and test stress values aiming at the defects of the prior art, and effectively and objectively evaluate the error between a simulation value (simulation stress value) and a test value (test stress value).
In order to solve the technical problems, the technical scheme adopted by the invention is as follows: a processing method of finite element simulation stress values and test stress values comprises the following steps:
1) calculating the absolute error between the simulated stress value and the test stress value;
2) calculating the utilization rate of the material, calculating the relative error between the simulated stress value and the test stress value by using the absolute error, and calculating the matching rate of the simulated stress value and the test stress value by using the relative error;
3) and drawing by taking the utilization rate of the material as an X axis and the matching rate as a Y axis to obtain the relationship among the simulated stress value, the test stress value and the allowable stress.
Correspondingly, the invention also provides a processing system of the finite element simulation stress value and the test stress value, which comprises the following steps:
the absolute error calculation module is used for calculating the absolute error between the simulation stress value and the test stress value;
the utilization rate calculating module is used for calculating the utilization rate of the material;
the matching rate calculation module is used for calculating the relative error between the simulated stress value and the test stress value by the absolute error and calculating the matching rate of the simulated stress value and the test stress value by using the relative error;
and the drawing module is used for drawing by taking the utilization rate of the material as an X axis and the matching rate as a Y axis to obtain the relationship among the simulated stress value, the test stress value and the allowable stress.
Compared with the prior art, the invention has the beneficial effects that: the method can obtain the utilization rate of the material by introducing the allowable stress of the material, obtain the matching rate through the relative error conversion between the test value and the simulation value, and visually observe the relationship among the test value, the simulation value and the allowable stress by drawing by taking the utilization rate as an X coordinate and taking the matching rate as a Y coordinate, thereby filling the blank in processing data at present; the method intuitively, accurately and reasonably expresses the relation between the test result and the simulation result, is associated with the actual application scene, is objective and is suitable for engineering application.
Drawings
FIG. 1 is a graph showing the results of the present invention.
Detailed Description
The invention specifically realizes the following steps:
firstly, obtaining a calculated value through finite element analysis or other calculation methods;
secondly, test data are obtained through tests;
thirdly, calculating the absolute error between the simulation value and the test value, and obtaining the absolute error through the calculation of a formula (1):
absolute error is an artificial value-test value (1)
Fourthly, calculating the utilization rate of the material, and obtaining the utilization rate through the calculation of a formula (2):
yield-test value/allowable stress (2)
And fifthly, calculating the relative error between the simulation value and the test value, and obtaining the error through a formula (3):
relative error ABS ((absolute error)/test value (3)
And sixthly, calculating the matching rate of the simulation value and the test value, and obtaining the result through the calculation of a formula (4):
match rate 1-relative error (4)
And sixthly, drawing by taking the material utilization rate obtained by the fourth step as an X coordinate and taking the matching rate of the simulated value and the test value obtained by the sixth step as a Y coordinate.
The material of the invention can be stainless steel, carbon steel, aluminum alloy and other materials used in static strength experiments.
Table 1 is obtained by EXCEL.
TABLE 1
Measuring point Test value Simulation value Allowable stress Absolute error Utilization rate Relative error Match rate
1 156.14 174.4 345 18.26 0.45 0.116946 0.883054
2 118.44 115.3 345 -3.14 0.34 0.026511 0.973489
3 -176.82 -181.2 345 -4.38 0.51 0.024771 0.975229
4 31.92 40.57 345 8.65 0.09 0.27099 0.72901
5 -21.84 -30.1 345 -8.26 0.06 0.378205 0.621795
66 -122.96 -114.4 355 8.56 0.35 0.069616 0.930384
67 300.2 318.9 355 18.7 0.85 0.062292 0.937708
68 24.64 25.92 345 1.28 0.07 0.051948 0.948052
69 -18.13 -24.53 345 -6.4 0.05 0.353006 0.646994
As can be seen from the table above, if a large number of test points with low matching rate are found in the region with high utilization rate, the test values and the simulation values are marked to have larger errors; and finding a large number of test points with lower matching rate in the area with low utilization rate, wherein the simulation value is available because the test value is far smaller than the allowable stress.

Claims (3)

1. A processing method of finite element simulation stress values and test stress values is characterized by comprising the following steps:
1) calculating the absolute error between the simulated stress value and the test stress value;
2) calculating the utilization rate of the material, calculating the relative error between the simulated stress value and the test stress value by using the absolute error, and calculating the matching rate of the simulated stress value and the test stress value by using the relative error; the utilization rate is the allowable stress of the test stress value/material; the relative error between the simulated stress value and the test stress value is ABS (absolute error)/test stress value; the matching rate is 1-relative error;
3) and drawing by taking the utilization rate of the material as an X axis and the matching rate as a Y axis to obtain the relationship among the simulated stress value, the test stress value and the allowable stress.
2. A method for processing finite element simulated stress values and test stress values according to claim 1, characterized in that the absolute error is simulated stress value-test stress value.
3. A system for processing finite element simulated stress values and test stress values, comprising:
the absolute error calculation module is used for calculating the absolute error between the simulation stress value and the test stress value; the utilization rate calculating module is used for calculating the utilization rate of the material; the utilization rate is the allowable stress of the test stress value/material;
the matching rate calculation module is used for calculating the relative error between the simulated stress value and the test stress value by the absolute error and calculating the matching rate of the simulated stress value and the test stress value by using the relative error;
the relative error between the simulated stress value and the test stress value is ABS (absolute error)/test stress value;
the matching rate is 1-relative error;
and the drawing module is used for drawing by taking the utilization rate of the material as an X axis and the matching rate as a Y axis to obtain the relationship among the simulated stress value, the test stress value and the allowable stress.
CN201711075619.9A 2017-11-06 2017-11-06 Method and system for processing finite element simulation stress value and test stress value Active CN107704714B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711075619.9A CN107704714B (en) 2017-11-06 2017-11-06 Method and system for processing finite element simulation stress value and test stress value

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711075619.9A CN107704714B (en) 2017-11-06 2017-11-06 Method and system for processing finite element simulation stress value and test stress value

Publications (2)

Publication Number Publication Date
CN107704714A CN107704714A (en) 2018-02-16
CN107704714B true CN107704714B (en) 2020-11-27

Family

ID=61178171

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711075619.9A Active CN107704714B (en) 2017-11-06 2017-11-06 Method and system for processing finite element simulation stress value and test stress value

Country Status (1)

Country Link
CN (1) CN107704714B (en)

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101902195A (en) * 2009-11-27 2010-12-01 华中科技大学 Method for modeling generator excitation system
US8442780B2 (en) * 2008-07-01 2013-05-14 The University Of Iowa Research Foundation Material property identification system and methods
CN104090861A (en) * 2013-02-20 2014-10-08 哈佛蒸汽锅炉检验和保险公司 Dynamic outlier bias reduction system and method
CN104318041A (en) * 2014-11-19 2015-01-28 山东理工大学 Torque tube stress intensity checking method for externally biased non-coaxial type cab stabilizer bar
JP2015127670A (en) * 2013-12-27 2015-07-09 三菱日立パワーシステムズ株式会社 Stress estimation method, system and program
CN105160135A (en) * 2015-10-08 2015-12-16 中国飞机强度研究所 Method for calculating consistency of test data and analytical data of test piece

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20050267615A1 (en) * 2004-03-05 2005-12-01 Lavash Bruce W System and method of virtual representation of folds and pleats

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8442780B2 (en) * 2008-07-01 2013-05-14 The University Of Iowa Research Foundation Material property identification system and methods
CN101902195A (en) * 2009-11-27 2010-12-01 华中科技大学 Method for modeling generator excitation system
CN104090861A (en) * 2013-02-20 2014-10-08 哈佛蒸汽锅炉检验和保险公司 Dynamic outlier bias reduction system and method
JP2015127670A (en) * 2013-12-27 2015-07-09 三菱日立パワーシステムズ株式会社 Stress estimation method, system and program
CN104318041A (en) * 2014-11-19 2015-01-28 山东理工大学 Torque tube stress intensity checking method for externally biased non-coaxial type cab stabilizer bar
CN105160135A (en) * 2015-10-08 2015-12-16 中国飞机强度研究所 Method for calculating consistency of test data and analytical data of test piece

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
Fast and accurate far-field evaluation from a non redundant, finite number of plane polar measurements;O.M. Bumf 等;《Proceedings of IEEE Antennas and Propagation Society International Symposium and URSI National Radio Science Meeting》;20020806;第540-543页 *
锻钢支撑座预锻模开裂失效分析与试验;周杰 等;《塑性工程学报》;20091028;第16卷(第5期);第36-40页 *

Also Published As

Publication number Publication date
CN107704714A (en) 2018-02-16

Similar Documents

Publication Publication Date Title
CN111008502B (en) Fault prediction method for complex equipment driven by digital twin
CN105608263B (en) A kind of adaptive processing method towards turbine blade structural life-time probability analysis
CN111291486B (en) Reliability evaluation method for system component of numerical control machine tool
CN110261247B (en) Synchronous characterization method for anisotropic yield and hardening constitutive parameters of metal material
CN108629114B (en) Assembly tolerance simulation analysis method for airplane assembly connection deformation
CN105868428A (en) Springback compensation method of stamped part
CN109299579B (en) Method for correcting wind tunnel force test data of large-aspect-ratio aircraft
CN112414668B (en) Wind tunnel test data static bomb correction method, device, equipment and medium
CN105005294A (en) Real-time sensor fault diagnosis method based on uncertainty analysis
CN107704714B (en) Method and system for processing finite element simulation stress value and test stress value
CN106405388B (en) A kind of digit chip function test method and system
CN111308327B (en) Analog circuit fault location and fault element parameter identification method
CN104166778A (en) Method for optimizing rigidity and damping of contact part of automobile seat guide rail
CN105488351A (en) Method for generating noise model of mobile electrocardiogram signal
CN101477582B (en) Model modification method for a semiconductor device
CN108021774B (en) Data processing method and device
CN107643472B (en) Method for calculating difference degree of short circuit break table
CN107063157A (en) A kind of method for building up of the automobile metal plate work frame of reference
CN110334459B (en) Rapid and refined modeling system and method for power transmission tower line system
CN105354374B (en) Rigidity simulation method and device for connection point
CN104268320A (en) Novel vibration isolator stiffness matrix rapid estimation method applicable to satellite sensitive loads
CN108196087B (en) Data processing apparatus
CN112632883B (en) Method, device, equipment and medium for testing simulation result of device model
CN113536460B (en) Aircraft multi-stage maintenance time verification data supplementing method and system
CN102903289B (en) A kind of test method of random render analog physical environment

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant