发明授权
- 专利标题: System and method for computing thermal boundary conditions from an unstructured CFD simulation on structural components
- 专利标题(中): 用于从结构化CFD模拟结构部件计算热边界条件的系统和方法
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申请号: US13592374申请日: 2012-08-23
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公开(公告)号: US09396296B2公开(公告)日: 2016-07-19
- 发明人: Vikram Singh Mangat , Jose-Angel Hernanz Manrique , Madhusudana Reddy , Punit Tiwari , Shreesh Mishra , Sunil Kumar , Sandhya Jha
- 申请人: Vikram Singh Mangat , Jose-Angel Hernanz Manrique , Madhusudana Reddy , Punit Tiwari , Shreesh Mishra , Sunil Kumar , Sandhya Jha
- 申请人地址: IN Bangalore, Karnataka
- 专利权人: AIRBUS ENGINEERING CENTRE INDIA
- 当前专利权人: AIRBUS ENGINEERING CENTRE INDIA
- 当前专利权人地址: IN Bangalore, Karnataka
- 代理机构: Global IP Services, PLLC
- 代理商 Prakash Nama
- 优先权: IN3058/CHE/2011 20110905
- 主分类号: G06F7/60
- IPC分类号: G06F7/60 ; G06F17/10 ; G06F17/50
摘要:
A system and method for computing thermal boundary conditions from an unstructured computational fluid dynamics (CFD) simulation for a thermal simulation of a structural component are disclosed. The thermal boundary conditions include convective heat transfer coefficient (HTC) and reference temperature (Tref). In one embodiment, prism cells are formed to capture boundary layer substantially next to a wall of the structural component. Further, tetrahedral cells are formed to capture a diffused temperature layer substantially next to the formed last prism cell and in a direction normal to the wall. Furthermore, temperature of each of the prism cells is computed in the direction normal to the wall until a substantially first tetrahedral cell. In addition, the computed temperature of the prism cell that is substantially adjacent to the first tetrahedral cell is declared as the Tref. Also, the HTC is computed using the obtained Tref.
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