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Effects of partial blockage inside film holes on overall cooling effectiveness of an integrated impingement-fin-film cooling configuration on blade pressure side
ZHOU Junhui, ZHANG Jingzhou
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2016, (9): 2729 -2738 .  DOI: 10.7527/S1000-6893.2016.0067

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341