Zobrazeno 1 - 9
of 9
pro vyhledávání: '"M A Gobran"'
Autor:
A F Nabhan, G Mburu, F Elshafeey, R Magdi, M Kamel, M Elshebiny, Y G Abuelnaga, M Ghonim, M H Abdelhamid, Mo Ghonim, P Eid, A Morsy, M Nasser, N Abdelwahab, F Elhayatmy, A A Hussein, N Elgabaly, E Sawires, Y Tarkhan, Y Doas, N Farrag, A Amir, M F Gobran, M Maged, M Abdulhady, Y Sherif, M Dyab, J Kiarie
Publikováno v:
Human Reproduction Open. 2022
STUDY QUESTION What is the scope of literature regarding women’s reproductive span in terms of definitions, trends and determinants? SUMMARY ANSWER The scoping review found a wide variation in definitions, trends and determinants of biological, soc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3300eab4d8a2b9b92c8aa9bab3abe667
https://doi.org/10.1093/hropen/hoac005
https://doi.org/10.1093/hropen/hoac005
Publikováno v:
QJM: An International Journal of Medicine. 113
Introduction Custodiol cardioplegia is attractive for minimally invasive cardiac surgery, as a single dose provides a long period of myocardial protection. Despite widespread use in Europe, there is little data confirming its efficacy compared with c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca729b779bab871fd4b76a3c7ea5fdf9
https://doi.org/10.1093/qjmed/hcaa042.004
https://doi.org/10.1093/qjmed/hcaa042.004
Publikováno v:
International Review of Aerospace Engineering (IREASE). 12:93
In this paper, the performance deterioration for the fan due to geometry changes by erosion is investigated and discussed. Furthermore, the fan life time is predicted. The fan in concern is installed in General Electric CF6-50 high bypass turbofan en
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::604a4d7be3a45a8bb46a06b3742563c0
https://doi.org/10.15866/irease.v12i2.16072
https://doi.org/10.15866/irease.v12i2.16072
Publikováno v:
International Journal of Performability Engineering. 15:2563
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ec22eaa8ae063fa3f79c998e5b6639bf
https://doi.org/10.23940/ijpe.19.10.p1.25632569
https://doi.org/10.23940/ijpe.19.10.p1.25632569
Publikováno v:
International Conference on Aerospace Sciences and Aviation Technology. 11:1-21
The present study deals with the air flow through an axial flow transonic fan blades, found in high bypass turbofan engines. Examples are CF-6, RB211 and GE90 turbofan engines. The fan has a wide chord, highly twisted blades of large span with a mean
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13c6db47ae81030fa547ca9249e6b89a
https://doi.org/10.21608/asat.2011.27139
https://doi.org/10.21608/asat.2011.27139
Autor:
M. H. Gobran
Publikováno v:
International Conference on Aerospace Sciences and Aviation Technology. 14:1-14
In the present paper, the aerodynamic characteristics of a single vertical cylinder as well as two vertical circular vertical cylinders aligned side-by-side (whose centerline is perpendicular to the flow), located in the incompressible flow field, ar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::89a1812ddb2b72f7e4564b214f0d2c4a
https://doi.org/10.21608/asat.2011.23433
https://doi.org/10.21608/asat.2011.23433
Publikováno v:
International Conference on Aerospace Sciences and Aviation Technology. 10:1-17
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7cb77752a7739402cee9f3bcd863fdf5
https://doi.org/10.21608/asat.2013.24413
https://doi.org/10.21608/asat.2013.24413
Publikováno v:
Volume 7: Turbomachinery, Parts A, B, and C.
A numerical model has been developed to study the impact of wet compression on the performance of three stages axial compressors. The CFD code, “FLUENT” was used to solve the governing equations in three dimensional, unsteady, turbulent flow sche
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3e0aa53aa5baa0e4e9fae33a4d1a6f9
https://doi.org/10.1115/gt2010-22079
https://doi.org/10.1115/gt2010-22079
Publikováno v:
International Review of Aerospace Engineering (IREASE). 7:17
In the present work, the three dimensional (3-D) flow field through the transonic axial flow fan and the intake of the CF6-50 high bypass ratio turbofan engine is investigated under the flight cruise conditions (11000 meter altitude and 0.85 Mach num
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea7e25a3f2b0c3859b3b28ccf8e0c4f3
https://doi.org/10.15866/irease.v7i1.1338
https://doi.org/10.15866/irease.v7i1.1338