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Study Over Thermal State of Gas Turbine Engine Metal-ceramic Rotor Blades and Nozzle Guide Vanes Und
[期刊论文] 作者：MOLCHANOV,B.V. SOUDAREV,
来源：Journal of Thermal Science 年份：2004
To ensure a reliable operation of the 2.5 MW gas turbine engine (GTE- 2.5) with the inlet gas temperature TIT = 1623 K, studies were performed over the thermal...
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