MARC details
| 000 -LEADER |
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| fixed length control field |
02372cam a2200313 a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
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| control field |
EG-GiCUC |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
160201s2015 ua o f m 000 0 eng d |
| 040 ## - CATALOGING SOURCE |
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| Original cataloging agency |
EG-GiCUC |
| Language of cataloging |
eng |
| Transcribing agency |
EG-GiCUC |
| 041 0# - LANGUAGE CODE |
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| Language code of text/sound track or separate title |
eng |
| 049 ## - LOCAL HOLDINGS (OCLC) |
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| Holding library |
Deposite |
| 097 ## - Thesis Degree |
|---|
| Thesis Level |
Ph.D |
| 099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC) |
|---|
| Classification number |
Cai01.13.11.Ph.D.2015.Mo.N |
| 100 0# - MAIN ENTRY--PERSONAL NAME |
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| Personal name |
Mohamed Morsy AbouRawash Abdelmo{u2019}ty |
| 245 10 - TITLE STATEMENT |
|---|
| Title |
Numerical investigations of gas turbine stage design configurations and Tip leakage / |
| Statement of responsibility, etc. |
Mohamed Morsy AbouRawash Abdelmo{u2019}ty ; Supervised Haytham Mourad Elzomor , Esmail Mohamed Elbialy |
| 246 15 - VARYING FORM OF TITLE |
|---|
| Title proper/short title |
دراسات عدديه لتصميم و تسرب الحافه لمرحله توربين غازى |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
|---|
| Place of publication, distribution, etc. |
Cairo : |
| Name of publisher, distributor, etc. |
Mohamed Morsy AbouRawash Abdelmo{u2019}ty , |
| Date of publication, distribution, etc. |
2015 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Extent |
127 P. : |
| Other physical details |
photographs ; |
| Dimensions |
30cm |
| 502 ## - DISSERTATION NOTE |
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| Dissertation note |
Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Mechanical Power Engineering |
| 520 ## - SUMMARY, ETC. |
|---|
| Summary, etc. |
Many experimental studies have been conducted until now to explore the details of aerodynamics and heat transfer inside the gas turbine engine. Due to limitations in the experimental facility, most of the experiments have been performed under non - realistic conditions such as low inlet / outlet pressure ratio, low inlet temperature, non rotating turbine blade which are far from the actual turbine operating condition. One of the most critical components of gas turbine engines, rotor blade tip, is exposed to high thermal loads. It is a significant challenge to the designer to protect the turbine material from this severe operating condition. Leakage flow over the blade tip is also one of the important issues to improve the turbine performance. High pressure gas turbine stage with real operating conditions was modelled and simulated using commercial CFD solver ANSYS FLUENT® 15.The modelled turbine stage has 46 vanes and 76 blades with a pressure ratio of 2.4 and a rotational speed of 12630 rpm. Depending on the validation, standard k-f model is employed; grid independency check exceeded 7.6 million elements |
| 530 ## - ADDITIONAL PHYSICAL FORM AVAILABLE NOTE |
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| Additional physical form available note |
Issued also as CD |
| 653 #4 - INDEX TERM--UNCONTROLLED |
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| Uncontrolled term |
Gas turbine |
| 653 #4 - INDEX TERM--UNCONTROLLED |
|---|
| Uncontrolled term |
Numerical investigations |
| 653 #4 - INDEX TERM--UNCONTROLLED |
|---|
| Uncontrolled term |
Rotating blade |
| 700 0# - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Esmail Mohamed Elbialy , |
| Relator term |
|
| 700 0# - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Haytham Mourad Elzomor , |
| Relator term |
|
| 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 |
