关注
Mohammed Khalil Ibrahim
Mohammed Khalil Ibrahim
Professor, Aerospace Engineering Department, Faculty of Engineering, Cairo University
在 eng.cu.edu.eg 的电子邮件经过验证
标题
引用次数
引用次数
年份
Mixing enhancement of compressible jets by using unsteady microjets as actuators
MK Ibrahim, R Kunimura, Y Nakamura
AIAA journal 40 (4), 681-688, 2002
672002
Design and navigation control of an advanced level CANSAT
S Ay, MK Ibrahim, ME Aydemır, M Bensaada, LHJDK Fernando, ...
Proceedings of 5th International Conference on Recent Advances in Space …, 2011
262011
Novel flow control method for vortex shedding of turbine blade
MM El-Gendi, MK Ibrahim, K Mori, Y Nakamura
Transactions of the Japan Society for Aeronautical and Space Sciences 53 …, 2010
202010
Experimental investigation of screech-tone characteristics of jet interaction with a flat plate
MK Ibrahim, T Sawai, K Obase, K Mori, Y Nakamura
AIAA journal 47 (9), 2031-2038, 2009
152009
Computational Fluid Dynamics Validation Study of Wake-Capturing Capability for Flat-Plate Wake
A Ochi, MK Ibrahim, Y Nakamura
Journal of aircraft 47 (2), 441-449, 2010
122010
Project-based space engineering education: Application to autonomous rover-back CanSat
H Aly, O Sharkawy, A Nabil, A Yassin, M Tarek, SM Amin, MK Ibrahim
2013 6th International Conference on Recent Advances in Space Technologies …, 2013
112013
Experimental and theoretical investigations of edge tones in high speed jets
MK Ibrahim
Journal of Fluid Science and Technology 8 (1), 1-19, 2013
112013
Design, fabrication, and realization of a supersonic wind tunnel for educational purposes
MK Ibrahim, AF Abohelwa, GB Salem
International Journal of Mechanical Engineering Education 37 (4), 286-303, 2009
102009
Spreading enhancement of axisymmetric supersonic jet by the use of micro jets
M Ibrahim, R Kunimura, Y Nakamura
15th AIAA Computational Fluid Dynamics Conference, 3048, 2001
92001
Effects of rotating tabs on flow and acoustic fields of supersonic jet
MK Ibrahim, Y Nakamura
AIAA journal 39 (4), 745-748, 2001
82001
Effects of tip cavity depth, width, and location on the leakage flow in an axial turbine cascade
M El-Ghandour, MK Ibrahim, K Doi, Y Nakamura
Journal of Fluid Science and Technology 5 (3), 558-573, 2010
72010
Energy separation in high subsonic turbine cascade
MM El-Gendi, MK Ibrahim, K Mori, Y Nakamura
Transactions of the Japan Society for Aeronautical and Space Sciences 52 …, 2010
72010
The Role of vortices in side jet/blunt body interaction at hypersonic speed
MK Ibrahim, T Nakamura, K Kitamura, K Mori, Y Nakamura
Transactions of the Japan Society for Aeronautical and Space Sciences, Space …, 2009
72009
The effects of vane-type tabs on flow and acoustic fields of supersonic jet
M Ibrahim, Y Nakamura
38th Aerospace Sciences Meeting and Exhibit, 87, 2000
62000
Experimental analysis of TSTO aerodynamic heating problems at hypersonic speed
H Ozawa, K Hanai, M Ibrahim, K Mori, Y Nakamura
15th AIAA International Space Planes and Hypersonic Systems and Technologies …, 2008
52008
On line splitting in the optimum tapered Burg algorithm
M Ibrahim
IEEE Transactions on Acoustics, Speech, and Signal Processing 35 (10), 1476-1479, 1987
51987
Control of Leakage Flow by Triple Squealer Configuration in Axial Flow Turbine
M El-Ghandour, MK Ibrahim, K Mori, Y Nakamura
Transactions of the Japan Society for Aeronautical and Space Sciences 53 …, 2010
42010
Comparison between hot and cold flow conditions of turbine cascade
MM El-Gendi, K Doi, MK Ibrahim, K Mori, Y Nakamura
Transactions of the Japan Society for Aeronautical and Space Sciences 53 …, 2010
42010
Contribution of UNISEC-global to capacity building in space engineering
MK Ibrahim, R Kawashima, AR Aslan
2017 8th International Conference on Recent Advances in Space Technologies …, 2017
32017
Towards understanding the physics of supersonic jet screech
I Menshov, I Semenov, I Ahmedyanov, MK Ibrahim, Y Nakamura
Computational Fluid Dynamics 2008, 101-106, 2009
32009
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