Radiation heat transfer model for complex superalloy turbine blade in directional solidiifcation process based on ifnite element method
turbine blade、radiation heat transfer、heat transfer model、simulation results、the Finite Element Method、heat capacity
13
TG249(铸造)
This research is ifnancialy supported by the Program for New Century Excelent Talents in UniversityNCET-13-0229, NCET-09-0396;the National Science & Technology Key Projects of Numerical Control2012ZX04010-031,2012ZX0412-011;the National High Technology Research and Development Program “863” Program of China2013031003
2016-05-18(万方平台首次上网日期,不代表论文的发表时间)
共10页
123-132