http://rdf.ncbi.nlm.nih.gov/pubchem/patent/KR-100393849-B1
Outgoing Links
Predicate | Object |
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classificationCPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentcpc/G01L1-00 |
classificationIPCInventive | http://rdf.ncbi.nlm.nih.gov/pubchem/patentipc/G01L1-00 |
filingDate | 2001-08-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
grantDate | 2003-08-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationDate | 2003-08-06-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
publicationNumber | KR-100393849-B1 |
titleOfInvention | Stress analysis method based on Mixed Volume and Boundary Integral Equation Method |
abstract | The present invention provides a volume-bound integral equation analysis for stress intensity factor analysis at the crack tip when a plurality of isotropic or anisotropic inclusions interacting with each other and an isotropic infinite or finite solid, including voids or cracks, are subjected to static and dynamic loads. A method of processing using: A first step of generating a volume-bound integral equation model using a finite element method preprocessor; Converting the data from the finite element method preprocessor into volume-bound integral equation input data; A third step of performing an analysis using a volume-bound integral equation program; A fourth step of converting the volume-bound integral equation analysis result into data capable of post-processing by a finite element post-processor; And a fifth step of performing post-treatment in the finite element post-processor.n n n Therefore, the stress intensity factor analysis at the crack tip can be effectively performed when static and dynamic loads are applied to the solid containing the inclusion and the cavity or the crack. |
priorityDate | 2001-08-27-04:00^^<http://www.w3.org/2001/XMLSchema#date> |
type | http://data.epo.org/linked-data/def/patent/Publication |
Incoming Links
Predicate | Subject |
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isDiscussedBy | http://rdf.ncbi.nlm.nih.gov/pubchem/substance/SID420500392 http://rdf.ncbi.nlm.nih.gov/pubchem/compound/CID21216988 |
Total number of triples: 12.