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COMPUTER MODELLING OF SHOCK INTERACTION OF THE LARGE BIRD WITH HIGH BYPASS RATIO TURBOFAN FAN BLADES
Publikováno v:
Авіаційно-космічна техніка та технологія, Vol 0, Iss 7, Pp 76-83 (2017)
As a result of the experimental-calculated analysis, and the analysis of consequences of real cases of collision with large birds domestic and foreign high bypass ratio turbofans, the calculated model of shock interaction of a large bird with high by
Externí odkaz:
https://doaj.org/article/4ded3e2f790e4ee3bb8471eeac5a50c7
