The Effect of Cooling-Air Flow Conditions on the Thermal State of High-Pressure Nozzle Blade
PROCEEDINGS OF 2019 INTERNATIONAL CONFERENCE ON SYSTEM SCIENCE AND ENGINEERING (ICSSE)（2019）
摘要
Developing technique utilized for cooling turbine blades plays an important role in designing as well as manufacturing Gas Turbine Engine (GTE). This may enhance the GTE's lifetime and decrease its fuel consumption. The paper numerically examines the effect of cooling-air mass flow rate and other flow conditions including temperature and pressure on the thermal state of high-pressure nozzle blade of the DR 76 gas turbine engine.
更多查看译文
关键词
CFD, cooling-air, GTE DR 76, nozzle blade, thermal state
AI 理解论文
溯源树
样例
生成溯源树，研究论文发展脉络
Chat Paper
正在生成论文摘要