Thermal analysis on the first stage turbinerotorblade has been completed based on the CFD results under calculated conditions.
根据某型涡喷发动机计算状态叶片流场计算结果，对该发动机高压涡轮转子叶片进行了热分析；
2
Tip clearance flow in a radial inflow turbinerotorblade under stage environment was investigated by 3-dimensional viscous flow simulation.
对微型燃机向心透平叶轮顶部间隙流动在级环境下进行了全三维粘性数值模拟。
3
This model accounts for the uncertainty about the loads acting on the wind-turbinerotorblade by the unstable wind distribution. A 20-year design lifetime is considered.