Genetic Algorithm-Based Fundamental Frequency Optimization of Laminated Composite Shells Carrying Distributed Mass (Record no. 17699)
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| 000 -LEADER | |
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| fixed length control field | a |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20220930154335.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 220930b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE | |
| Original cataloging agency | AIKTC-KRRC |
| Transcribing agency | AIKTC-KRRC |
| 100 ## - MAIN ENTRY--PERSONAL NAME | |
| 9 (RLIN) | 7513 |
| Author | Pal, S. |
| 245 ## - TITLE STATEMENT | |
| Title | Genetic Algorithm-Based Fundamental Frequency Optimization of Laminated Composite Shells Carrying Distributed Mass |
| 250 ## - EDITION STATEMENT | |
| Volume, Issue number | Vol, 103(3), June |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. | |
| Place of publication, distribution, etc. | Kolkatta |
| Name of publisher, distributor, etc. | Springer |
| Year | 2022 |
| 300 ## - PHYSICAL DESCRIPTION | |
| Pagination | 389–401p |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | Composite plates and shells are an inevitable part of the modern structural, aerospace and marine industry. Load-carrying plates and shells must be optimized from a frequency viewpoint to avoid resonance. In the present study, a global optimization framework is developed by combining the iterative improvement ability of genetic algorithm (GA) with the brute accuracy of finite element (FE) method to optimize the fundamental frequency of composite shells. Since composites are weak in shear, the shear deformation effect is considered by using the first-order shear deformation theory in the finite element formulation. The ply angles are considered as the design variables. However, only discrete ply angles with 5° increments in the ± 90° search space are considered. Various numerical studies are carried out to check the validity and accuracy of the present FE-GA approach. A wide range of results for rectangular and cylindrical shell panels with different radius of curvatures, boundary conditions and carrying distributed mass at different positions are presented. |
| 650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| 9 (RLIN) | 4626 |
| Topical term or geographic name entry element | Mechanical Engineering |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| 9 (RLIN) | 10825 |
| Co-Author | Kalita, K |
| 773 0# - HOST ITEM ENTRY | |
| Title | Journal of the institution of engineers (India): Series C |
| International Standard Serial Number | 2250-0545 |
| Place, publisher, and date of publication | Kolkata Institution of Engineers (India) |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| URL | https://link.springer.com/article/10.1007/s40032-021-00801-9 |
| Link text | Click here |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | Dewey Decimal Classification |
| Koha item type | Articles Abstract Database |
| Withdrawn status | Lost status | Source of classification or shelving scheme | Damaged status | Not for loan | Home library | Current library | Shelving location | Date acquired | Total Checkouts | Barcode | Date last seen | Price effective from | Koha item type |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dewey Decimal Classification | School of Engineering & Technology | School of Engineering & Technology | Archieval Section | 30/09/2022 | 2022-1767 | 30/09/2022 | 30/09/2022 | Articles Abstract Database |