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Job Description We are looking for a heat transfer engineer to be responsible for turbine blades and vanes heat transfer calculation and cooling design for heavy duty gas turbine development. What are my responsibilities?You will be responsible for gas turbine hot path parts design including heat transfer and friction correlations, Impingement cooling, film cooling, & compressible flow design to fulfill the turbine performance requirements defined in product requirement specificationsClosely work within turbine blades and vanes design integrated project team with different disciplines including aerodynamics, second air system engineering, mechanical design, mechanical integrity, material and manufacturing. What do I need to qualify for this job?Master’s degree or above in mechanical engineering, thermal engineering, aeronautical engineering or turbomachinery5 years or above working experience in various gas turbine vane and blades heat transfer design Familiar with heat transfer and friction correlations, impingement cooling, film cooling and compressible flow. Hands-on experience on 1D flow network analysis.Familiar with design modeling tools such as NX, 3D CFD Pre-Processing tools, commercial or in-house aerodynamics and heat transfer calculation tools such as CFX. Good understanding on turbine blades and vanes manufacturing and mechanical integrity.Proficient in idea generation and be able to transfer know-how or search for outside available sources to various contexts and solve difficult technical problems independentlyStrong interpersonal skills to work with multi-cultural colleagues, customers, industry experts, and university associates.Good teamwork, ownership and results orientedGood communication and presentation skills.Professional proficiency in English language