Numerical Investigation of the dynamic performance of a supersonic intake with variable geometry/ (Record no. 167875)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 03371namaa22004211i 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 005 - أخر تعامل مع التسجيلة | |
| control field | 20250223033258.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 240916s |||||||f |m|| 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 | Deposite |
| 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.2023.Lu.N |
| 100 0# - MAIN ENTRY--PERSONAL NAME | |
| Authority record control number or standard number | Lubna Abdelaal Arafa Hassan Margha, |
| Preparation | preparation. |
| 245 10 - TITLE STATEMENT | |
| Title | Numerical Investigation of the dynamic performance of a supersonic intake with variable geometry/ |
| Remainder of title | Remainder of title / |
| Statement of responsibility, etc. | by Lubna Abdelaal Arafa Hassan Margha; Prof. Dr. Aly Abdel Fattah Hashem, Dr. Ahmed Tawfeek El-Taweel. |
| 246 15 - VARYING FORM OF TITLE | |
| Title proper/short title | التحقق العددي للأداء الديناميكي لمدخل أسرع من الصوت مع تصميم هندسي متغير |
| 264 #0 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Date of production, publication, distribution, manufacture, or copyright notice | 2023. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 98 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, 2023. |
| 504 ## - BIBLIOGRAPHY, ETC. NOTE | |
| Bibliography, etc. note | Bibliography: pages 89-94. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | The phenomenon of dynamic transition between the regular reflection and Mach reflection<br/>is studied at M∞ = 3, 3.5,& 4. A new technique is proposed to study the phenomenon by<br/>controlling the wedge’s inclination angle. The present work aims to implement numerical<br/>simulations of the moving trailing edge of an inviscid wedge while the throat area is maintained<br/>fixed. The third part of the current research aims to investigate the gain in performance<br/>and pressure ratio when the single ramp is rapidly divided into two ramps. The first<br/>one is kept stationary while the other one is rotated with a trailing edge low Mach number. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc. | تمت دراسة ظاهرة الانتقال الديناميكي بين الانعكاس المنتظم وانعكاس ماخ عند ماخ للتدفق الحر = 3 و 3.5 و 4. تم اقتراح تقنية جديدة لدراسة الظاهرة من خلال التحكم في زاوية ميل الإسفين. يهدف الجزءان الأولان من العمل الحالي إلى تنفيذ عمليات محاكاة لتحريك الإسفين غير المربوط مع الحفاظ على منطقة الحلق ثابتة. يهدف الجزء الثالث من البحث الحالي إلى التحقيق في الزيادة في الأداء ونسبة الضغط عندما يتم تقسيم المنحدر الفردي بسرعة إلى منحدرين. الأول يبقى ثابتًا بينما الآخر يتم تدويره برقم ماخ منخفض الحافة الخلفية. |
| 530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE | |
| Issues CD | Issued 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 |
| Source of heading or term | qrmak |
| 653 #0 - INDEX TERM--UNCONTROLLED | |
| Uncontrolled term | Dynamic shock |
| -- | Moving double ramps |
| -- | Supersonic intake |
| -- | Mach reflection |
| -- | Regular reflection |
| 700 0# - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Aly Abdel Fattah Hashem |
| Relator term | thesis advisor. |
| 700 0# - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Ahmed Tawfeek El-Taweel |
| Relator term | thesis advisor. |
| 900 ## - Thesis Information | |
| Grant date | 01-01-2023 |
| Supervisory body | Aly Abdel Fattah Hashem, Prof. Dr. Aly Abdel Fattah Hashem |
| Discussion body | Dr. Mohammed Khalil Ibrahim, Prof. Dr. Ahmed Farouk AbdelGawad |
| Universities | Cairo University |
| Faculties | Faculty of Engineering |
| Department | Department of Aerospace |
| 905 ## - Cataloger and Reviser Names | |
| Cataloger Name | Samah |
| Reviser Names | Huda |
| 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 | 16.09.2024 | 88532 | Cai01.13.01.M.Sc.2023.Lu.N | 01010110088532000 | 16.09.2024 | 16.09.2024 | Thesis |