Analytical and experimental improvement of flutter performance of plate wings using piezoelectric patches / (Record no. 172667)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 03694namaa22004211i 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 005 - أخر تعامل مع التسجيلة | |
| control field | 20250621123148.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 250621s2024 ua a|||frm||| 000 0 eng d |
| 040 ## - CATALOGING SOURCE | |
| Original cataloguing agency | EG-GICUC |
| Language of cataloging | eng |
| Transcribing agency | EG-GICUC |
| Modifying agency | EG-GICUC |
| Description conventions | rda |
| 041 0# - LANGUAGE CODE | |
| Language code of text/sound track or separate title | eng |
| Language code of summary or abstract | eng |
| -- | ara |
| 049 ## - Acquisition Source | |
| Acquisition Source | Deposit |
| 082 04 - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 629.47 |
| 092 ## - LOCALLY ASSIGNED DEWEY CALL NUMBER (OCLC) | |
| Classification number | 629.47 |
| Edition number | 21 |
| 097 ## - Degree | |
| Degree | M.Sc |
| 099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC) | |
| Local Call Number | Cai01.13.01.M.Sc.2024.Ge.M |
| 100 0# - MAIN ENTRY--PERSONAL NAME | |
| Authority record control number or standard number | George Barsoum Saad Barsoum, |
| Preparation | preparation. |
| 245 10 - TITLE STATEMENT | |
| Title | Analytical and experimental improvement of flutter performance of plate wings using piezoelectric patches / |
| Statement of responsibility, etc. | by George Barsoum Saad Barsoum ; Supervisors Prof. Hani M. Negm, Dr. Mohamed A. Mahran. |
| 246 15 - VARYING FORM OF TITLE | |
| Title proper/short title | دراسة تحليلية ومعملية لتحسين سرعة الرفرفة للأجنحة بإستخدام الشرائح الذكية / |
| 264 #0 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Date of production, publication, distribution, manufacture, or copyright notice | 2024. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 120 pages : |
| Other physical details | illustrations ; |
| Dimensions | 30 cm. + |
| Accompanying material | CD. |
| 336 ## - CONTENT TYPE | |
| Content type term | text |
| Source | rda content |
| 337 ## - MEDIA TYPE | |
| Media type term | Unmediated |
| Source | rdamedia |
| 338 ## - CARRIER TYPE | |
| Carrier type term | volume |
| Source | rdacarrier |
| 502 ## - DISSERTATION NOTE | |
| Dissertation note | Thesis (M.Sc)-Cairo University, 2024. |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE | |
| Bibliography, etc. note | Bibliography: pages 105-108. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | This study is concerned with aeroelastic flutter control of straight wings using piezoelectric patches. The research encompasses analytical, numerical, and experimental approaches to assess the dynamic characteristics of plate wings, and evaluate optimal control strategies for mitigating flutter instabilities.<br/>The work incorporates analytical techniques using Ritz method. Subsequently, a finite element model (FEM) is developed to analyze static, modal,implicit and flutter behavior of plate wings with different piezoelectric arrangements. A Linear Quadratic Regulator- LQR incorporating piezoelectric patches is designed and implemented to increase flutter speed of straight plate wings |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | هذه الدراسة تهتم بالتحكم في سرعة الرفرفة للجناح باستخدام منظومتين من الشرائح الذكية على نماذج من الألواح الصلب للجناح. تم استنتاج سرعة الرفرفة باستخدام طرق تحليلية للجناح بدون شرائح ذكية وطرق عددية بتطوير وبرمجة خوارزميات طريقة العناصر المحدودة لطبقات اللوح مع الشرائح الذكية، وتم إستنتاج الخصائص الديناميكية والاهتزازات وحدوث ظاهرة الرفرفة.<br/>تم اختبار لوح الجناح معمليا في معمل الديناميكا الهوائية واختبار الخصائص الديناميكية بمعمل ديناميكا الهياكل. وبناءا عليه تم تطوير وبرمجة وعمل خوارزميات لتصميم منظومة التحكم الأمثل وتم استخدام الخوارزميات الچينية لاختيار القيم المثلى لبارامترات المتحكم لزيادة سرعة الرفرفة بإستخدام منظومتين مختلفتين من الشرائح الذكية. |
| 530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE | |
| Issues CD | Issues also as CD. |
| 546 ## - LANGUAGE NOTE | |
| Text Language | Text in English and abstract in Arabic & English. |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | Spacecraft Engineering |
| Source of heading or term | qrmak |
| 653 #0 - INDEX TERM--UNCONTROLLED | |
| Uncontrolled term | Aeroelastic control |
| -- | Piezoelectric |
| -- | Vibration control |
| -- | Finite element Model |
| 700 0# - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Hani M. Negm |
| Relator term | thesis advisor. |
| 700 0# - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Mohamed A. Mahran |
| Relator term | thesis advisor. |
| 900 ## - Thesis Information | |
| Grant date | 01-01-2024 |
| Supervisory body | Hani M. Negm |
| -- | Mohamed A. Mahran |
| Discussion body | Gamal M. El-Bayoumi |
| -- | Mostafa A. Ahmed Elshafei |
| Universities | Cairo University |
| Faculties | Faculty of Engineering |
| Department | Department of Aerospace Engineering |
| 905 ## - Cataloger and Reviser Names | |
| Cataloger Name | Shimaa |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | Dewey Decimal Classification |
| Koha item type | Thesis |
| Edition | 21 |
| Suppress in OPAC | No |
| Source of classification or shelving scheme | Home library | Current library | Date acquired | Inventory number | Full call number | Barcode | Date last seen | Effective from | Koha item type |
|---|---|---|---|---|---|---|---|---|---|
| Dewey Decimal Classification | المكتبة المركزبة الجديدة - جامعة القاهرة | قاعة الرسائل الجامعية - الدور الاول | 21.06.2025 | 91678 | Cai01.13.01.M.Sc.2024.Ge.M | 01010110091678000 | 21.06.2025 | 21.06.2025 | Thesis |