Students graduated with accumulative undergraduate marks 65% or higher are legible to apply for the degree of Master of Science, and subsequently for the Doctor of philosophy degree. Students graduated with accumulative undergraduate marks less than 65% are legible to apply for the Diploma.
| The Aerospace Department offers three postgraduate degrees: | ||
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Diplomas | |
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Aerospace Engineering | |
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Airplane Design | |
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Propulsion / Rockets Diploma | |
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Air Transport Diploma | |
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Master of Science | |
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Doctor of Philosophy | |
Research Fields
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| Aerodynamics | ||
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Unsteady Aerodynamics & Aeroacoustics | |
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Indoor Air Flows & Environmental Aerodynamics | |
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Flow Control & Reduced Order Modeling | |
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Wind Energy & Wind Turbine Design | |
| Flight Mechanics & Control | ||
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Aircraft Control Systems | |
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Satellite Attitude Dynamics & Control | |
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Missile Navigation, Guidance & Control | |
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Advanced Control (Robust, Fuzzy,…) | |
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Robot Dynamics & Control | |
| Structures | ||
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Finite Element Analysis | |
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Dynamics of Structures | |
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Aeroelsaticity | |
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Composite Materials | |
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Smart Structures | |
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Design Optimization | |
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Management of Engineering Systems | |
| Propulsion | ||
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Multivariable control of gas turbine engines. | |
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Gas turbine engine diagnostics. | |
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Compressor surge prediction and control. | |
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Computational analysis of compressor cascades under surge conditions. | |
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Modeling of reacting flows. | |
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Numerical simulation of unsteady combustion. | |
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Development of general procedure for constructing reduced reaction mechanisms. | |
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Effect of droplet atomization on flow characteristics. | |
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Interactions of fuel type-droplet formation effects on pollution. | |
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Evaluation of droplet shape effect on combustion stability. | |
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Hybrid rocket propulsion. | |
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Numerical modeling of composite propellant combustion. | |
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Modeling of catalyst bed reactors. | |
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Modeling of Pulsed plasma thrusters. | |
Courses: