机译:高温热障涂层的Sylramic-IBN /热解碳/化学气相渗透碳化硅陶瓷基质复合行为在燃烧环境中
Department of Aeronautics and Astronautics Air Force Institute of Technology Wright-Patterson AFB Ohio USA;
Structural Materials Division 97042 Materials and Manufacturing Directorate Air Force Research Laboratory Wright-Patterson AFB Ohio USA;
Department of Aeronautics and Astronautics Air Force Institute of Technology Wright-Patterson AFB Ohio USA;
Structural Materials Division 97042 Materials and Manufacturing Directorate Air Force Research Laboratory Wright-Patterson AFB Ohio USA;
Structural Materials Division 97042 Materials and Manufacturing Directorate Air Force Research Laboratory Wright-Patterson AFB Ohio USA;
Burner rig; ceramic matrix composite; combustion environment; environmental barrier coatings; high temperature;
机译:高温热障涂层的Sylramic-IBN /热解碳/化学气相渗透碳化硅陶瓷基质复合行为在燃烧环境中
机译:通过化学蒸汽渗透法改善碳化硅纤维增强碳化硅基质复合材料的导热率
机译:化学气相渗透法制备的颗粒增强碳化硅与氮化硅陶瓷基复合材料的组织与性能
机译:化学蒸汽渗透碳纤维增强碳化硅基复合材料的力学性能和微观结构特性
机译:碳化硅基质表面复合材料的热梯度化学气相渗透。
机译:硅衬底的电导率和取向对热化学气相沉积合成多壁碳纳米管的影响
机译:压力脉冲反应化学气相沉积法制备用于陶瓷基复合材料的纳米级多层多孔碳化物中间相
机译:快速化学气相渗透法制备陶瓷纤维 - 陶瓷基复合材料