HEAT TRANSFER IN HIGH-PRESSURE COMPRESSOR GAS TURBINE INTERNAL AIR SYSTEMS: A ROTATING DISC-CONE CAVITY WITH AXIAL THROUGHFLOW

Author： Alexiou A.   Hills N. J.   Long C. A.   Turner A. B.   Millward J. A.  

Publisher： Taylor & Francis Ltd

ISSN： 1521-0480

Source： Experimental Heat Transfer, Vol.13, Iss.4, 2000-10, pp. : 299-328

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