Senin, 06 Juni 2011

Research Studentship in Turbine Rotor Blade Cooling


College Scholarship Money Therefore, foreign students must provide the difference between UK / EU and overseas student rate for the cost of the University from several other sources, such as scholarships or private funds.
- A first or second class honors degree above or equivalent in engineering or related discipline (materials, applied mathematics, physics);
- Interest in the turbine and heat transfer / cooling technology;
-Experience in computing (eg Fortran, Pascal, Matlab or similar)
- Good oral and written communication skills, including ability to write in English at a standard suitable for the preparation of written reports, publications and verbal presentation of work at the level of generalists and specialists;
- Excellent record of academic achievement and / or professional
The following skills desirable but not essential:
- Experience in collaborative work with researchers to turbines research engineer.

Open Scholarship for International Students: None

College Scholarship Money Description: Students will work closely with colleagues in the research group in Thermo-Fluids Laboratory at the House Southwell (Osney Mead) and the Rolls Royce to research new system for cooling the blades used in the future of High Pressure Turbine jet engine. http://www.callforpapersinfo.com
http://thescholarshipprogramme.com
Stage high pressure turbine rotor of a gas turbine is one of the most sophisticated system of mechanical engineering in modern aircraft. College Scholarship Money Knives must operate for thousands of hours and experience that exceed the gas temperature and spun at 12,000 1600oC rpm produces centrifugal stresses that produce blade root load of about 18tonnes. This project will research new technologies for use in future machines.
College Scholarship Money Working with engineers at Oxford and Rolls-Royce, students will determine the operating conditions of the turbine blade in the future of large civil engines; candidates cooling technology review and propose new systems that are suitable for turbine blades, turbine cooling system design and produce computer models; design and conduct experiments, analyze the data.

How to Apply: Online

Scholarship Application Deadline: June 10, 2011

Further Scholarship Information and Application