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The research scope of GTT includes efforts to increase reliability, efficiency and power output of gas turbines and aero engines. The most important areas of research are the following: fluid-structure interaction at forced response and flutter for turbine and compressor blades, cooling techniques for gas turbine blades, flow control using plasma.
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Name
2014_ERCOFTAC Bulletin 101.pdf
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restricted
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31.26 MB
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Adobe PDF
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8e9636a6bf5d275ce06aa97f26a2e12a