2021
DOI: 10.1007/s12046-021-01707-z
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Multi-objective design optimization of turbine blade leading edge for enhanced aerothermal performance

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Cited by 2 publications
(1 citation statement)
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“…Therefore, one purpose in the literatures to optimize the turbine blade structure was stress minimization [1] .The complexity of turbine blade structure brings great difficulties to parametric optimization. However, the optimization of turbine blades is extremely complicated [11][12] . Many studies are based on local optimization, such as fir-tress [1] , film holes [13] , blade profile, leading edge [14] , blade Tip [15] .…”
mentioning
confidence: 99%
“…Therefore, one purpose in the literatures to optimize the turbine blade structure was stress minimization [1] .The complexity of turbine blade structure brings great difficulties to parametric optimization. However, the optimization of turbine blades is extremely complicated [11][12] . Many studies are based on local optimization, such as fir-tress [1] , film holes [13] , blade profile, leading edge [14] , blade Tip [15] .…”
mentioning
confidence: 99%