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Improving dynamic and aeroelastic performance of helicopter rotors using periodic design and piezo active control / (Record no. 67240)

MARC details
000 -LEADER
fixed length control field 02501cam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223032037.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 180902s2018 ua dh 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.Ho.I
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Hossam Taha Abdelaziz Ahmed Badran
245 10 - TITLE STATEMENT
Title Improving dynamic and aeroelastic performance of helicopter rotors using periodic design and piezo active control /
Statement of responsibility, etc. Hossam Taha Abdelaziz Ahmed Badran ; Supervised Hani M. Negm , Mohammad Tawfik
246 15 - VARYING FORM OF TITLE
Title proper/short title تحسين الأداء الدينامى و المرونة الهوائية لدوار الهليكوبتر باستخدام التصميم الدوري و التحكم التلقائى بالمواد الكهربية الإجهادية
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Hossam Taha Abdelaziz Ahmed Badran ,
Date of publication, distribution, etc. 2018
300 ## - PHYSICAL DESCRIPTION
Extent 127 P. :
Other physical details charts , facsimiles ;
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 study, we improve the vibration characteristics of sandwich helicopter rotor blades with periodic changes in the core material. This technique preserves the external geometry of the rotor blades to keep their aerodynamic characteristics.Since the construction and air velocity change along the rotor blade, we use the finite element technique in its dynamical and aeroelastic analyses. Theodorsen's 2-D thin airfoil theory with a lift deficiency function is used in the unsteady aerodynamic analysis, with a correction which takes into consideration that each blade falls in the wake of the preceding blade. Results of the analyses show significant improvement in the dynamic response and flutter speeds of helicopter rotors in both hovering and forward flight, as a result of using the periodic design technique of the blades. Introducing piezoelectric smart material in the core design of the blades together with active automatic control is shown to further improve the dynamic characteristics of the helicopter rotor
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Helicopter rotors
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Periodic design
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Vibration attenuation
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Hani Mohammad Elmorsy Negm ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Mohammad Tawfik Aboelsooud ,
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 Enas
Reviser Cataloger
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Nazla
Reviser Revisor
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.Ho.I 01010110075428000 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.Ho.I 01020110075428000 22.09.2023 CD - Rom 75428.CD