Ground and wall effects on a hovering flapping airfoil / (Record no. 172397)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 03871namaa22004331i 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 005 - أخر تعامل مع التسجيلة | |
| control field | 20250706122414.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 250528s2024 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 | 629.1 |
| 092 ## - LOCALLY ASSIGNED DEWEY CALL NUMBER (OCLC) | |
| Classification number | 629.1 |
| Edition number | 21 |
| 097 ## - Degree | |
| Degree | M.Sc |
| 099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC) | |
| Local Call Number | Cai01.13.01.M.Sc.2024.Mo.G |
| 100 0# - MAIN ENTRY--PERSONAL NAME | |
| Authority record control number or standard number | Mohamed Ehab Ibrahim Khalil, |
| Preparation | preparation. |
| 245 10 - TITLE STATEMENT | |
| Title | Ground and wall effects on a hovering flapping airfoil / |
| Statement of responsibility, etc. | by Mohamed Ehab Ibrahim Khalil ; Supervision Prof. Dr. Mohamed Madbouli Abdel Rahman, Prof. Dr. Amr Gamal Guaily. |
| 246 15 - VARYING FORM OF TITLE | |
| Title proper/short title | تأثيرات الأرض والجدار على الجنيح المرفرف المحلق |
| 264 #0 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Date of production, publication, distribution, manufacture, or copyright notice | 2024. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 144 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 141-144. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | The target of the thesis is to study the ground and wall effects on a two-dimensional flapping wing hovering in an inclined stroke plane. To achieve so, a finite element FORTRAN code has been developed to solve the Navier-Stokes equations, the developed code has been coupled with an Eulerian technique utilized in capturing the position of the flapping airfoil, in addition to developing a force calculation algorithm. The developed code has been validated against benchmark problems, and the hovering flapping airfoil model results have been compared with published work. Simulations for the ground and side wall effects on a flapping airfoil hovering in an inclined stroke plane have been conducted. Then a parametric study with the ground effect has been conducted over the parameters of the hovering flapping airfoil. Then an enhancement for the ground effect is proposed. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | الهدف من هذه الرسالة هو دراسة تأثيرات الأرض والجدار على جناح مرفرف ثنائي الأبعاد يحلق في مستوى مائل. ولتحقيق ذلك، تم تطوير كود بلغة الفورتران ذو العناصر المحدودة لحل معادلات نافيير-ستوكس، ويقترن الكود المطور بتقنية أويلر المستخدمة في التقاط موضع الجنيح المرفرف، بالإضافة إلى تطوير خوارزمية حساب القوة. تم التحقق من صحة الكود الذي تم تطويره بمقارنة نتائجه بنتائج مسائل معروفة ، وتمت مقارنة نتائج نموذج الجنيح المرفرف المحلق مع النتائج المنشورة سابقا. تم إجراء محاكاة لتأثير الأرض والجدار على الجنيح المرفرف الذي يحلق في مستوى مائل. ومن ثم أجريت دراسة بارامترية مع التأثير الأرضي على متغيرات الجنيح المرفرف المحلق. ثم تم إجراء تحسين للتأثير الأرضي. |
| 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 | Aerospace Engineering |
| Source of heading or term | l c subject heading |
| 650 #7 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | هندسة الفضاء |
| Source of heading or term | qramk |
| 653 10 - INDEX TERM--UNCONTROLLED | |
| Uncontrolled term | Flapping Airfoil |
| -- | Hovering |
| -- | Navier-Stokes Equations |
| -- | Finite Element Method |
| -- | Inclined Stroke Plane |
| 700 0# - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Mohamed Madbouli Abdel Rahman |
| Relator term | thesis advisor. |
| 700 0# - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Amr Gamal Guaily |
| Relator term | thesis advisor. |
| 900 ## - Thesis Information | |
| Grant date | 01-01-2024 |
| Supervisory body | Mohamed Madbouli Abdel Rahman |
| -- | Amr Gamal Guaily |
| Discussion body | Gamal Mahmoud El-Bayoumi |
| -- | Ahmed Farouk Abdelgawad |
| 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 | 28.05.2025 | 91347 | Cai01.13.01.M.Sc.2024.Mo.G | 01010110091347000 | 28.05.2025 | 28.05.2025 | Thesis |