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Scheduling variable stator vanes of axial flow compressor / (Record no. 82923)

MARC details
000 -LEADER
fixed length control field 02036cam a2200301 a 4500
003 - CONTROL NUMBER IDENTIFIER
control field EG-GiCUC
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 211101s2021 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.2021.Ra.S
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Rami Mtanios Alturk
245 10 - TITLE STATEMENT
Title Scheduling variable stator vanes of axial flow compressor /
Statement of responsibility, etc. Rami Mtanios Alturk ; Supervised Ali Abdelfattah Hashem
246 15 - VARYING FORM OF TITLE
Title proper/short title {u200C}جدولة دوران الريش الثابتة للضواغط المحورية{u٢٠٠أ}
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Cairo :
Name of publisher, distributor, etc. Rami Mtanios Alturk ,
Date of publication, distribution, etc. 2021
300 ## - PHYSICAL DESCRIPTION
Extent 152 P. :
Other physical details charts , fsacsimiles ;
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 study is presented in four parts: First, An optimization process was carried out to design an axial flow compressor using a genetic algorithm where a Simple radial equilibrium model was adopted. Second, a code has been implemented that can do the off-design of multistage axial flow compressors using radial variation design.The compressor map was evaluated in the direct version. Third, a methodology was developed to study the effect of inlet guide vane (IGV) and variable stator vanes (VSVs) on the performance of the axial compressor. Fourth, schedule of (VSVs). Before introducing VSVs technique, the surge margin of the axial flow compressor in the case study vanished at a non-dimensional rotational speed of 80%. Applying the VSVs technique, the surge free operation was extended to a non-dimensional rotational speed of 65%.This is adequate because in practice gas turbine engines non dimensional idle speed is close to 67%
530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE
Additional physical form available note Issued also as CD
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Axial Flow Compressor
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Transonic
653 #4 - INDEX TERM--UNCONTROLLED
Uncontrolled term Variable Stator Vanes
700 0# - ADDED ENTRY--PERSONAL NAME
Personal name Ali Abdelfattah Hashem ,
Relator term
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Nazla
Reviser Revisor
905 ## - LOCAL DATA ELEMENT E, LDE (RLIN)
Cataloger Shimaa
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.M.Sc.2021.Ra.S 01010110084612000 22.09.2023 Thesis  
Dewey Decimal Classification   المكتبة المركزبة الجديدة - جامعة القاهرة مخـــزن الرســائل الجـــامعية - البدروم 11.02.2024 Cai01.13.01.M.Sc.2021.Ra.S 01020110084612000 22.09.2023 CD - Rom 84612.CD