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Professor/أستاذ:Mohammed Khalil Ibrahim
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Aeronautics and Aerospace Engineering
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| | Professor | |
| Email : | MKHALIL***eng.cu.edu.eg |
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| Mobile : | +20-1006764242 |
| Work Phone : | +20-2-35678653 |
| Room Number : | 40203 |
| Fax : | +20-2-35723486 |
| Home Page : | http://scholar.cu.edu.eg/mkhalil |
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| Qualifications |
|  B.Sc. (1991) "Aerospace Engineering" The University of Cairo (Egypt) |
| M.Sc. (1996) "Aerospace Engineering" The University of Cairo (Egypt) |
| Ph.D. (2002) "Aerospace Engineering" Nagoya University (Japan) |
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| Fields of Interest : |
| Experimental Fluid Dynamics (EFD) |
| Computational Fluid Dynamics (CFD) |
| Aeroacoustics & Flow Induced Noise and Vibration |
| Fluid-Structural Interaction |
| Propulsion Systems and Heat Transfer |
| Flow Control |
| Flow Visualization |
| Pressure and Temperature Sensitive Paints (PSP & TSP) |
| Wind and Renewable Energy |
| Automatic Control of Autonomous VTOL Aircraft |
| Nano-satellites and remote sensing |
| Measurement Technology |
| Space Engineering Education |
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| Recent Publications : |
| -2014-IBRAHIM, M. K., N. Miya, K. Mori, and Y. Nakamura, "Experimental Investigation of Noise and Flow Characteristics of Supersonic Underexpanded Jet Interaction with a Coannular Tube", The Transaction of The Japan Society for Aeronautical and Space Sciences. |
| -2013-IBRAHIM, M. K., "Image Processing-Based Technique for Computation of Axial Sound Source Distribution in a Chocked Screech Jet", International Review of Aerospace Engineering (IREASE), vol. 6, issue 1, pp. 76-82. |
| -2013-BRAHIM, M. K., "Experimental and Theoretical Investigation on Edge Tones in High Speed Jets", ”, Journal of Fluid Science and Technology, vol. 8, issue 1, pp. 1-19. |
| -2011-Mohammed K. Ibrahim, Soichiro Matsumoto, Koichi Mori and Yoshiaki NAKAMURA, “Visualization of Pressure Field over Rotating Blades using Pressure Sensitive Foil Technique" , The Transaction of The Japan Society for Aeronautical and Space Sciences, Vol. 53, No. 182, pp. 243–249, 2011. |
| -2010-Koichi MORI, Yoshiki MURAHASHI, Yutaka KOGA,Yoshiaki NAKAMURA, Mohammed K. IBRAHIM , Takashi TAKAHASHI , Keiichi MURAKAMI, Takashi AOYAMA , and Atsushi HASHIMOTO, “A simple technique for the precise measurement of transmission loss of planar sound waves”, AIAA Journal Vol. 48, No.10, October 2010, pp. 2377-2385. |
| -2010-Mohamed EL-GHANDOUR, Mohammed K. IBRAHIM, Katsunori DOI, and Yoshiaki NAKAMURA, "Effects of Tip Cavity Depth, Width, and Location on the Leakage Flow in an Axial Turbine Cascade", Journal of Fluid Science and Technology, Vol. 5, No. 3, Nov. 2010, pp. 558-573. |
| -2010-Mahmoud El-Gendi, Mohammed K. Ibrahim, Koichi Mori, Yoshiaki Nakamura, Comparison Between Hot and Cold Flow Conditions of a Turbine Cascade”, Transaction of Japan Society for Aeronautical and Space Sciences, Vol. 53, No. 181, Nov. 2010, pp. 171-179. |
| -2010-Mahmoud El-Gendi, Mohammed K. Ibrahim, Koichi Mori, Yoshiaki Nakamura, “Novel Flow Control Method of Vortex Shedding for a Turbine”, The Transaction of The Japan Society for Aeronautical and Space Sciences, Vol. 53, No. 180, 2010, pp. 122–129. |
| -2010-Mohamed El-Ghandour, Mohammed K. Ibrahim, Koichi Mori, Yoshiaki Nakamura, “Control of Leakage Flow by Triple Squealer Configuration in Axial Flow Turbine”, The Transaction of The Japan Society for Aeronautical and Space Sciences, Vol. 53, No. 179, pp. 1–7, 2010. |
| -2010-Ochi, A. Mohammed K. Ibrahim, and Nakamura, Y. “Computational Fluid Dynamics Validation Study of Wake-Capturing Capability for Flat-Plate Wake", Journal of Aircraft, Vol. 47, No. 2, pp 441-449, 2010. |
| -2010-Mahmoud El-Gendi, Mohammed K. Ibrahim, Koichi Mori, Yoshiaki Nakamura, “Energy Separation in a High Subsonic Turbine Cascade”, Transaction of The Japan Society for Aeronautical and Space Sciences, Vol. 152, No. 47, pp. 206-212, 2010. |
| -2010-Design Supersonic Test Facilities, Nagoya University, Japan |
| -2009-Mohammed K. Ibrahim, Tetsuya Nakamura, Keiichi Kitamura, Koichi Mori and Yoshiaki Nakamura, “The Role of Vortices in Side Jet/Blunt Body Interaction at Hypersonic Speed”, Trans. JSASS Space Tech. Japan, Vol. 7 (2009), pp.1-10 . |
| -2009-Ochi, A. Mohammed K. Ibrahim, and Nakamura, Y. “CFD Validation Study of Wake Capturing Capability for Flat Plate Wake”, AIAA Journal of Aircraft, 2009. (in Press) |
| -2009-Mohammed K. Ibrahim, A. Abohelwa, and Galal B. Salem “Design, Fabrication Testing of a Supersonic Wind Tunnel for Educational Purposes”, International journal of mechanical engineering education, Manchester University, UK, Vol. 37, No. 4, pp. 286-303, 2009. |
| -2009-Mohammed K. Ibrahim, Takashi Sawai, Kimihito Obase, Koichi Mori, and Yoshiaki Nakamura, “Experimental Investigation of Screech-Tone Characteristics of Jet Interaction with a Flat Plate”, AIAA Journal, Vol. 47, No. 9, pp. 2031-2038, 2009. |
| -2002-Mohammed K. Ibrahim, and Nakamura, Y. "Correlation between linear stability theory and transition of compressible jet shear layer," The transaction of Japan Society for Aeronautical and Space Sciences, JSASS, Vol. 45, No. 147, May 2002, pp 35-44. |
| -2002-Mohammed K. Ibrahim, Kunimura, R. and Nakamura, Y. "Mixing Enhancement of Compressible Jets by Using Unsteady Micro-Jets as Actuator," AIAA Journal, Vol 40, No. 4, 2002, pp. 681-688. |
| -2002-Mohammed K. Ibrahim, and Nakamura, Y. "Effects of Rotating Tabs on Flow and Acoustic Fields of Supersonic Jet," AIAA journal Vol. 39, no 4, 2001, pp.745-748 |
| -1997-Mohammed K. Ibrahim, and El-Haggar, S.M. "Parametric Study of Solar Hydrogen Production From Saline Water Electrolysis," International Journal of Environment and Pollution, Vol. 8, Nos. 1-2, pp. 164-173, 1997. |
| Recent Projects : | | --Design, Fabrication and Realization of an Acoustic Test Facility for Noise and Vibration Study of Space Launching System. (2007 – 2010) Funded by Japan Aerospace Exploration Agency, Tokyo, Japan
| | --Development of Numerical Flow Solver for The Prediction of Flow Induced Load on Building (2004-2005) Funded by The Steel Network, Inc., North Carolina, USA
| | --Design , Fabrication and Realization of Engineering System for Air Defense Application (2003 – 2012)
Funded by Research, Development, Technology, Design Center, Ministry of Military Production, Egypt
| | --Development of Turbulent Model of Internal Flow Applications. (2005-2007) Funded by Densotechno Corporation, Nagoya, Japan
| | --Development of Test Rig for The Application of Pressure Sensitive Paint for Turbo-Machine Application (2006 – 2007) Funded by Centre of Excellence (COE), School of Engineering, Nagoya University, Japan
| | --Development of New Pressure Sensitive Paint Technique for Turbo-Machine Application (2007 – 2009) Funded by Mitsubishi Heavy Industries, Ltd., Nagoya, Japan
| | --Design, Fabrication and Realization of Miniature Unmanned Air Vehicle (UAV) (2006 – 2009)Funded by Equos Research Co., Ltd, Nagoya, Japan.
| | --Modeling and Analysis of Hot-Dip Galvanizing Line (2008-2009) Funded by Nippon Steel Corporation, Chiba, Japan.
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| Recent Books : | | --CanSat-Based Space Engineering Education, UNISEC, 2012 |
| Recent Courses : | | --AER 201A Basic Fluid Mechanics | | --AER 201B Gas Dynamics | | --AER 301B Boundary Layer Theory | | --AER 401 High Speed Aerodynamics | | --AER 450 Airplane Flight Performance | | --AER 474 Airplane Design | | --AER 602A Panel Methods | | --AER 602 Experimental Methods in Engineering | | --AER 615 Experimental Methods in Aerodynamics | | --AER 620 Advanced topics in Aerodynamics | | --AER 607 Hydrodynamics Stability | | --AE 313 Systems and Control | | --AE 426 Flight Dynamics | | --AE 421 Aerospace Engineering Labratory II | | --AE 520 Compressible Flow |
| Graduate Students : | | -2010-Mahmoud El-GENDI, Ph.D. “Numerical Simulation of Trailing Edge Vortex Shedding in a High Subsonic Turbine Cascade”, Minia University. | | -2010-Mohamed El-GHANDOUR, Ph.D. “A Triple Squealer For Axial Flow Turbines”, Nagoya University. | | -2009-Nobuhiro MIYA, M.Sc., “Experimental Study on Sound Suppression from Supersonic Jet Using Perforated Tubes”, Nagoya University.
| | -2009-Yutaka KOGA, M.Sc., “Experiments on Sound Transmission Characteristics with Acoustically Induced Vibration of Aluminum Thin plates and Honeycomb”, Nagoya University. | | -2007-Takashi SAWAI, M.Sc., “Experimental Investigation of Jet Interaction with Flat Plate on Screech Tone Characteristics”, Nagoya University. | | -2007-Tsutomu YABASHI, M.Sc., “Study of Basic Nose Configuration for Reduction of Sonic Boom”, Nagoya University.
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| Conferences : | | -2011-Celebi, M. Mohammed K. IBRAHIM, Aydemir, M.E., Bensaada M., Fernando L. H. J. D. K., Akiyama, H., Yamaura, S. “ Design and Navigation Control of an Advanced Level CANSAT”, 5th International Conference on Recent Advances in Space Technologies (RAST), 2011, 9-11 June 2011, pp/ 856-860, Istanbul, Turkey. | | -2011-Samy M. Amin , Hassan Ali Hassan, Omar M. EL Boughdady, Mohammed K. IBRAHIM, “Egyptian Space Science and Technology Educational Project Based on Can-Sat Program (CLTP)”, 3rd Nano-satellite Symposium, Kita-Kyushu, Kyushu Institute of Technology, 12th-14th December 2011. | | -2011-Rei Kawashima, Alim Rustem Aslan, Fernando Stancato, Hector Bedon Monzon, John Mugwe, Mohammed K. Ibrahim, Vidmantas Tomkus, Esau Vicente Vivas, Fernando Aguado-Agelet, Seiko Shirasaka, Robert Van Zyl, Shinichi Nakasuka, “Results and Future Perspective of the Mission Idea Contest”, ”, 3rd Nano-satellite Symposium, Kita-Kyushu, Kyushu Institute of Technology, 12th-14th December 2011. | | -2010-Mahmoud M. El-GENDI, Magdy BASSILY, Mohammed K. IBRAHIM, and Yoshiaki NAKAMURA, "Effect of Turbulence Model on the Calculated Flow through Rectilinear Turbine Cascade" accepted for publication in the second International Conference of Energy Engineering; ICEE-2, 27-29 December 2010, Aswan, Egypt. | | -2009-Mohammed K. Ibrahim, Koichi Mori , and Yoshiaki Nakamura, “Visualization of Flow Field over Rotating Blades using Pressure Sensitive Foil Technique”, 47th AIAA Aerospace Sciences Meeting and Exhibit, World Center Marriott Orlando, Florida, 5-8 January 2009, AIAA-2009-1076. USA. | | -2009-Nobuhiro Miya, Takaaki Yumitori, Mohammed K. Ibrahim, Kathunori Doi, Kouichi Mori and Yoshiaki Nakamura, “Noise suppression of supersonic jet due to a finite cylinder”, Russia-Japan biannual joint Symposium on CFD, Russia, 2009. | | -2009-Yoshiki Murahashi, Yutaka Koga, Mohammed K. Ibrahim, Koichi Mori, Yoshiaki Nakamura, Takashi Takahashi, Keiichi Murakami, Takashi Aoyama, Atsushi Hashimoto, “Experiments on Transmission Characteristics of CFRP with Plane Acoustic Waves”, 40th Annual Meeting of Japan Society of Aerospace and Space Sciences, Tokyo, 9-10 April 2009, Japan. | | -2008-Mahmoud El-Gendi, Mohammed K. Ibrahim, Koichi Mori, Yoshiaki Nakamura, “Elliptic Trailing Edge for a High Subsonic Turbine Cascade”, KSAS-JSASS Joint International Symposium on Aerospace Engineering, 20-21 November, 2008, Ramada Plaza Jeju Hotel , Jeju, Korea. | | -2008-Mohamed El-Ghandour, Mohammed K. Ibrahim, Koichi Mori, Yoshiaki Nakamura, “A Triple Squealer For Axial Flow Turbines”, KSAS-JSASS Joint International Symposium on Aerospace Engineering, 20-21 November, 2008, Ramada Plaza Jeju Hotel , Jeju, Korea. | | -2008-Igor Menshov, Ilya Semenov, Ildar Ahmedyanov, Mohammed Khalil Ibrahim, Yoshiaki Nakamura, “Towards Understanding the Physics of Supersonic Jet Screech”, The Fifth International Conference of Computational Fluid Dynamics – ICCFD5, Seoul, KOREA July 7-11, 2008. | | -2008-Mohammed K. Ibrahim, Koichi Mori , and Yoshiaki Nakamura, “Application of Pressure Sensitive Foil Technique to Visualize Subsonic Jet Flow over a Plate”, 13th International Conference on Applied Mechanics and Mechanical Engineering, AMME-13, May 27-29, 2008, Cairo, Egypt. | | -2008-Hiroshi Ozawa, Katsuhisa Hanai, Mohammed K. Ibrahim, Koichi Mori and Yoshiaki Nakamura, “Experimental Analysis of TSTO Aerodynamic Heating Problems at Hypersonic Speed”, AIAA Paper 2008-2671, 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, April 28 - May 1, 2008, Dayton Convention Center, Dayton, Ohio, USA. | | -2007-Ochi, A. Mohammed K. Ibrahim, and Nakamura, Y. “CFD Validation Study of Wake Capturing Capability for Flat Plate Wake”, ," 37th AIAA Fluid Dynamics Conference & Exhibit, 25-28 June 2007, Anaheim, CA, AIAA Paper 2007-4195, USA. | | -2007-Mahmoud El-Gendi, Mohammed K. Ibrahim, Koichi Mori, and Yoshiaki Nakamura, “Numerical Simulation of Trailing Edge Vortex Shedding in a High Subsonic Turbine Cascade”, JSASS-KSAS Joint International Symposium on Aerospace Engineering, October 10-12, 2007, Kitakyushu, Japan. | | -2007-Mohammed K. Ibrahim, “Visualization of Underexapnded Jet Flows over a Plate by Pressure-Sensitive Paint Technique”, 12th International Conference on Aerospace Sciences and Aviation Technology, May 29-31, 2007 Cairo, Egypt. | | -2001-Mohammed K. Ibrahim, Souma, T., and Nakamura, Y. "Suppression of Edge-Tones in High-Speed Flows," JSASS 5th International Sessions in 39th Aircraft Symposium October 29-31, 2001, Nagaragawa Convention Center, Gifu, Japan. | | -2001-Mohammed K. Ibrahim, Kunimura, R. and Nakamura, Y. "Spreading Enhancement of Axisymmetric Supersonic Jet by the Use of Micro Jets," 31st AIAA Fluid Dynamics Conference & Exhibit, 11-14 June 2001, Anaheim, CA, AIAA Paper 2001-3048, USA. | | -2000-Mohammed K. Ibrahim, and Nakamura, Y. "Flow Field and Noise Characteristics due to Supersonic Jet Shear Layer-Vortex Interaction," AIAA Fluids 2000 Conference and Exhibit, 19-22 June 2000, Denver, Colorado, AIAA Paper 2000-2533, USA. | | -2000-Mohammed K. Ibrahim, and Nakamura, Y. "The Effects of Vane-Type Tabs on Flow and Acoustic Fields of Supersonic Jet," 38th Aerospace Sciences Meeting & Exhibit, 10-13 Jan 2000, Reno, NV, AIAA Paper 2000-0087, USA. | | -1999-Mohammed K. Ibrahim, and Nakamura, Y. " Suppression of Supersonic Jet Noise by Free-to-Rotate Vane-Type Tabs," JSASS 13th International Session in 37th Aircraft Symposium, Ota-Ku Sangyo Plaza, 13-15 October 1999 ,Tokyo, Japan. | | -1997-Sherif, A. O. and Mohammed K. Ibrahim, "Grid Type Effects on Two-Dimensional Euler Computation," Proceeding of Al-Azhar Engineering Fifth International Conference, Cairo AEIC'97, Dec. 19-22, 1997, Egypt. | | -1995-Mohammed K. Ibrahim, and Sherif, A. O. "A Two-Dimensional Flux Vector Splitting Euler Solver," Proceeding of fifth International Conference of Fluid Mechanics, Cairo, ICFM5 Vol. II (1995), pp. 621-635, Egypt. |
| Administrative Positions : | | -2010-Chief Technical Officer, CTO, Transtechno-Egypt, LLC | | -2005-Administrative Manager, The Steel Network - Egypt, LLC | | -2004-Aerospace Engineering Department Secretariat |
| Awards : | | -2012-Cairo University International Publication Award | | -2011-Cairo University International Publication Award | | -2011-Who's Who in the World 2011. | | -2011-Cairo University, Fcaulty of Engineering, Award for Research Excellence | | -2010-Cairo University International Publication Award, May 2010 and October 2010. | | -2009-Cairo University International Publication Award. | | -2008-Best Paper and Presentation at 45th Annual Meeting of Japan Society of Aeronautical and Space Science, Nagoya. | | -1997-Cairo University Distinguish Young Researcher Award. | | -1990-Academic Outstanding Award, Cairo University. |
| Membership in Scientific Societies : | | --American Institute of Aeronautics and Astronautics (AIAA), Senior Member since 1999 | | --Japan Society for Aeronautical and Space Sciences (JSASS), Member since 2001 | | --University Space Engineering Consortium(UNISEC), Member since 2011 | | --Egyptian Engineers Syndicate, Member since 1991 |
| Invited lectures : | | -2011-Space Engineering Education in Egypt, University of Tokyo, Japan | | -2011-Recent Development in Nano-Satellites, King Fahd University of Petroleum and Minerals, KSA | | -2010-Noise Pollution and Control, American University In Cairo, Egypt | | -2008-Pressure Senstive Paints, COE, Nagoya University, Japan |
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