| Citation: | FENG Guomiao, LI Guoqing, BAI Xiaohui, et al. Film cooling characteristics and loss mechanism of combined construct with expansive main hole and contractive secondary holes[J]. Journal of Aerospace Power, 2026, 41(3):20240770 doi: 10.13224/j.cnki.jasp.20240770 |
Film cooling characteristics and aerodynamic loss mechanism were numerically simulated under a mainstream Mach number of 0.6. Three-cylindrical combination holes, variable cross-section cylin-drical combination holes and crescent combination holes were compared at the blowing ratio varying from 0.5 to 2.0. In a crescent combination holes with expansive main hole and contractive secondary holes, main-stream penetration was prevented in the mid-expansion hole. As for the side-contraction holes, the anti-kidney vortex was promoted due to acceleration. The mixing structure was changed due to different pre-ssure gradients of holes. When the blowing ratio was 1.5 and 2.0, compared with three-cylindrical combi-nation holes, the film cooling effectiveness increased by 17.8% and 29.7%, respectively, and the mixing pressure loss due to film cooling declined by 51% and 43%, respectively, in crescent combination holes.
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