MARC details
| 000 -LEADER |
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| fixed length control field |
02283cam 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 |
180415s2017 ua dh 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 |
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| Thesis Level |
M.Sc |
| 099 ## - LOCAL FREE-TEXT CALL NUMBER (OCLC) |
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| Classification number |
Cai01.13.01.M.Sc.2017.Ah.N |
| 100 0# - MAIN ENTRY--PERSONAL NAME |
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| Personal name |
Ahmed Ali Mahmoud Hussien |
| 245 10 - TITLE STATEMENT |
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| Title |
Numerical investigation of flow parameters and con guration of gas injection thrust vector control / |
| Statement of responsibility, etc. |
Ahmed Ali Mahmoud Hussien ; Supervised Aly Abdelfattah Hashem , Farouk Mohamed Owis |
| 246 15 - VARYING FORM OF TITLE |
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| Title proper/short title |
دراسة عددية لتأثير متغيرات حقن الغاز على التحكم في متجه الدفع |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. |
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| Place of publication, distribution, etc. |
Cairo : |
| Name of publisher, distributor, etc. |
Ahmed Ali Mahmoud Hussien , |
| Date of publication, distribution, etc. |
2017 |
| 300 ## - PHYSICAL DESCRIPTION |
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| Extent |
119 P. : |
| Other physical details |
charts , facsimiles ; |
| Dimensions |
30cm |
| 502 ## - DISSERTATION NOTE |
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| Dissertation note |
Thesis (M.Sc.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering |
| 520 ## - SUMMARY, ETC. |
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| Summary, etc. |
Thrust vector control is an e ective method of ying vehicle's directional control. Thrust vectoring using gas injection is attractive as it eliminates the need for complex mechanical systems such as gimbaled nozzles and jet vanes. The current thesis presents a numerical study to investigate the e ect of di erent parameters on the performance of secondary gas injection thrust vector control. The steady three dimensional Reynolds Averaged Navier Stokes equations are solved using the nite volume method on unstructured grid. The injection location, mass ow rate, and angle of the secondary injection are varied to examine their e ect on the thrust vectoring performance. Moreover, di erent injection ori ce shapes are investigated. The e ect of the temperature and the injected gas type are also studied. Thrust ratio, axial thrust augmentation factor, and ampli cation factors are calculated in order to be used in comparing the performance. The indicated parameters have to be precisely adjusted to maximize the thrust vectoring performance |
| 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 |
Parametric Study |
| 653 #4 - INDEX TERM--UNCONTROLLED |
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| Uncontrolled term |
Secondary Injection |
| 653 #4 - INDEX TERM--UNCONTROLLED |
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| Uncontrolled term |
Thrust Vector Contro |
| 700 0# - ADDED ENTRY--PERSONAL NAME |
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| Personal name |
Aly Abdelfattah Hashem , |
| Relator term |
|
| 700 0# - ADDED ENTRY--PERSONAL NAME |
|---|
| Personal name |
Farouk Mohamed Owis , |
| Relator term |
|
| 905 ## - LOCAL DATA ELEMENT E, LDE (RLIN) |
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| Cataloger |
Nazla |
| Reviser |
Revisor |
| 905 ## - LOCAL DATA ELEMENT E, LDE (RLIN) |
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| Cataloger |
Shimaa |
| Reviser |
Cataloger |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
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| Source of classification or shelving scheme |
Dewey Decimal Classification |
| Koha item type |
Thesis |
