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252 积分 2026-01-24 加入
Modeling and Performance Analysis of Variable Cycle Engine with Ceramic Matrix Composite Turbine Blades
1个月前
已完结
Evaluation of the relationship between the aerothermodynamic process and operational parameters in the high-pressure turbine of an aircraft engine
1个月前
已关闭
Study of design methods and heat transfer characteristics of combined cooling structure for turbine blades with turbine inter-vane burner
1个月前
已关闭
Aerothermal performance of cavity tip with flow structure effects in a transonic high-pressure turbine blade
1个月前
已完结
The scale-adaptive simulation of reverse coupling of aero-engine high pressure high-pressure turbine to combustion chamber flow
1个月前
已完结
3D-printing process design of lattice compressor impeller based on residual stress and deformation
1个月前
已完结
Corrosion mechanism investigation of TiN/Ti coating and TC4 alloy for aircraft compressor application
1个月前
已完结
Flow structure coupling LSTM-MOGA method in the unsteady aeroelastic optimization design of the compressor blade of the civil aircraft engine
1个月前
已关闭
Design and Numerical Analysis of an Annular Combustion Chamber
1个月前
已完结
Effects of combustor wall cooling structure on combustor performances
1个月前
已完结