header

Elastic and aeroelastic analysis of aircraft metallic, composite, and smart wings / (Record no. 70472)

MARC details
000 -LEADER
fixed length control field 01792cam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223032216.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 190224s2018 ua dho f m 000 0 eng d
040 ## - CATALOGING SOURCE
Original cataloging agency EG-GiCUC
Language of cataloging eng
Transcribing agency EG-GiCUC
041 0# - LANGUAGE CODE
Language code of text/sound track or separate title eng
049 ## - LOCAL HOLDINGS (OCLC)
Holding library Deposite
097 ## - Thesis Degree
Thesis Level Ph.D
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC)
Classification number Cai01.13.01.Ph.D.2018.Mo.E
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Mohamed Abdou Mahran Kasem
245 10 - TITLE STATEMENT
Title Elastic and aeroelastic analysis of aircraft metallic, composite, and smart wings /
Statement of responsibility, etc. Mohamed Abdou Mahran Kasem ; Supervised Hani M. Negm , Adel M. Elsabbagh
246 15 - VARYING FORM OF TITLE
Title proper/short title تحليل المرونه و المرونه الهوائيه للأجنحة المعدنية و المركبة ذات التراجع مع وجود مواد ذكيه كهربيه اجهادية
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Mohamed Abdou Mahran Kasem ,
Date of publication, distribution, etc. 2018
300 ## - PHYSICAL DESCRIPTION
Extent 103 P. :
Other physical details charts , facsimiles , photographs ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. In the present dissertation elastic and aeroelastic models are developed for the analysis of metallic and composite wings with attached piezoelectric actuators using the finite element method. The elastic and aeroelastic problems were modeled as eigenvalue problems. The piezoelectric potential effect is integrated as prestresses using the concept of geometric stiffness. The analysis covers 2-D and 3-D wings, and the effect of engine mass
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Aeroelasticity
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Finite elements
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Smart materials
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Adel M. Elsabbagh ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Hani M. Negm ,
Relator term
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="http://172.23.153.220/th.pdf">http://172.23.153.220/th.pdf</a>
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Nazla
Reviser Revisor
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Samia
Reviser Cataloger
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme Dewey Decimal Classification
Koha item type Thesis
Holdings
Source of classification or shelving scheme Not for loan Home library Current library Date acquired Full call number Barcode Date last seen Koha item type Copy number
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة قاعة الرسائل الجامعية - الدور الاول 11.02.2024 Cai01.13.01.Ph.D.2018.Mo.E 01010110077263000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.Ph.D.2018.Mo.E 01020110077263000 22.09.2023 CD - Rom 77263.CD