Japan Aerospace Exploration Agency (JAXA)Office of Space Flight and Operations Environmental and Structural Test Lab2-1-1 Sengen Tsukuba Ibaraki Japan 300-8505 ando.shigemasa@jaxa.jp;
Japan Aerospace Exploration Agency (JAXA)Office of Space Flight and Operations Environmental and Structural Test Lab2-1-1 Sengen Tsukuba Ibaraki Japan 300-8505 shi.qinzhong@jaxa.jp;
Japan Aerospace Exploration Agency (JAXA)Office of Space Flight and Operations Environmental and Structural Test Lab2-1-1 Sengen Tsukuba Ibaraki Japan 300-8505 nagahama.kenta@jaxa.jp;
Japan Aerospace Exploration Agency (JAXA)Office of Space Flight and Operations Environmental and Structural Test Lab2-1-1 Sengen Tsukuba Ibaraki Japan;
Japan Aerospace Exploration Agency (JAXA)Office of Space Flight;
Acoustic loads; Honeycomb Panel; Acoustic test; Randomvibration analysis; Statistical Energy Approach; Lossfactor; Sound radiation efficiency; artificial satellite; vibration attenuation of loading mass;
机译:用于声学诱导的蜂窝面板随机振动的外推技术
机译:随机不规则蜂窝芯夹芯板的自由振动分析
机译:双曲蜂窝夹芯板对随机声激励的动态响应。第1部分:实验研究
机译:安装在蜂窝面板上的设备随机声振动的预测
机译:平面蜂窝夹芯板的振动和声学性能
机译:振动和声学测量数据集用于实验室制动器设置中的尖叫声分析里昂中央大学(Ecole Centrale de Lyon)产生的摩擦引起的振动和噪音(FIVE @ ECL)
机译:堆蜂窝板的声加载振动响应分析。