Study on the thermal protection performance of superalloy honeycomb panels in high-speed thermal sho

• 作 者: Dafang Wu Anfeng Zhou Liming Z
• 机 构: SchoolofAeronauticSc-ienceandEngineering,SchoolofAstronautics
• 出 处: 力学快报：英文版
• 发表日期: 2014年2期
• 关键词: 热防护性能 高温合金 蜂窝板 冲击环境 三维有限元方法 防护设计 蜂窝结构 模拟系统 superalloy honeycomb panel thermal s
• 基金项目: This work was supported by the National Natural Science Foundation of China （11172026 and 91216301） and the Specialized Research Fund for the Doctoral Program of Higher Education （20131102110014）.

The thermal protection performance of superalloy honeycomb structure in high-temperature environments are important for thermal protection design of high-speed aircrafts. By using a self-developed transient aerodynamic thermal simulation system, the therm