Qusai Al-Hamdan

Lecturer in: Aircraft Hydraulic and Pneumatic Systems; Introduction to Aircraft Propulsion Systems, Aircraft Propulsion and Power Transfer Systems, Airframe and Propulsion Systems 1; Aircraft Engineering Project 2, Airframe and Propulsion Systems 2

Gas Turbine Engines Design, Modelling, Simulation, Component Matching and Testing.
Instrumentation and Data Acquisition Techniques for component and system testing.

Technical Projects

• Designing and building a computerised static firing test cell to test the actual performance of Ground to Air HAWK missile rocket engine.
• Upgrading Mirage F1 turbojet engine test cell by computerising the test cell, adding real time data acquisition system and automating some required test procedures.
• Upgrading a Modular Engine Test Cell (METS) used to test various turboprop and turbo-shaft engines including Rolls Royce T56, Lycoming T53 and Allison 250 engines by computerising the test cell, adding real time Data Acquisition system and automating some required test procedures.
• Upgrading fuel nozzle test bench by computerising the test bench, adding real time Data Acquisition system and automating some test procedures.
• Designing and building the requirements of upgrading Pratt & Whitney F100 engine test cell.

PhD (Gas Turbine Engines), University of Hertfordshire, UK
BSc (Mechanical Engineering), Mu’tah University, Jordan