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Static and dynamic stability of hingeless helicopter blade in hover / (Record no. 56209)

MARC details
000 -LEADER
fixed length control field 01864cam a2200337 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20250223031501.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 160427s2015 ua d 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 M.Sc
099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC)
Classification number Cai01.13.01.M.Sc.2015.Ah.S
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Ahmed Abdelmonem Ahmed Hussein
245 10 - TITLE STATEMENT
Title Static and dynamic stability of hingeless helicopter blade in hover /
Statement of responsibility, etc. Ahmed Abdelmonem Ahmed Hussein ; Supervised Gamal Mohammed Elbayoumi , Samir Mostafa Elkholy
246 15 - VARYING FORM OF TITLE
Title proper/short title الاستقرار السكونى و الحركى لريشة طائرة هيليكوبتر لامفصلية أثناء التحويم
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Ahmed Abdelmonem Ahmed Hussein ,
Date of publication, distribution, etc. 2015
300 ## - PHYSICAL DESCRIPTION
Extent 117 P. :
Other physical details charts ;
Dimensions 30cm
502 ## - DISSERTATION NOTE
Dissertation note Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering
520 ## - SUMMARY, ETC.
Summary, etc. The main objective of the thesis is to investigate the nonlinear geometric effects on the static and dynamic stability of helicopter hingeless rotor in hover. this nonlinearity mainly arises frrm the contribution of the flap and lead-lag bending to the elastic twist. the unsteady aerodynamic model was adapted to include the effect of both the pulsating free stream ans the returning spiral wake. differernt deficiency functions were used; quasi steady C(k) = 1, theodorsen C(k) and lowey C' (k,m.h) both divergence and flutter phenomena were studied
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Helicopter hovering
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Hingeless Rotor Blad
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Nonlinear trim Equations
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Gamal Mohammed Elbayoumi ,
Relator term
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Samir Mostafa Elkholy ,
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 Aml
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.M.Sc.2015.Ah.S 01010110068668000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.M.Sc.2015.Ah.S 01020110068668000 22.09.2023 CD - Rom 68668.CD