Detailed heat transfer distributions of narrow impingement channels for cast-in turbine airfoils
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American Institute of Aeronautics and Astronautics2012
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The mean value of turbine entry temperature increased to improve efficiency and specific power. Due to the combustor characteristics, thermal and aero-dynamics non-uniformities can be individuated at the turbine inlet section. Then, a further increase in t ...
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American Soc Mechanical Engineers, Three Park Avenue, New York, Ny 10016-5990 Usa2010
