机译:气孔发动机遏制中多相STF浸渍Kevlar织物的弹道冲击性能
Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;
Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;
Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;
Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;
Nanjing Univ Aeronaut & Astronaut Coll Energy & Power Engn Aeroengine Thermal Environm & Struct Key Lab Minist Ind & Informat Technol Nanjing 210016 Peoples R China;
Containment casing; Kevlar fabric; Shear thickening fluid; Ballistic impact; Rheological behavior; Yarn pull-out;
机译:预张力对燃气轮机安全壳系统多层Kevlar 49机织弹道冲击性能的影响
机译:多相STF浸渍Kevlar织物的宏观数值模拟方法。 第2部分:材料模型和数值模拟
机译:纱线拉出作为一种消散Kevlar〜(〜R)KM-2织物弹道冲击能的机制第二部分:预测弹道性能
机译:Kevlar 49和Zylon在代表喷气发动机风扇遏制的条件下的弹道冲击响应
机译:弹道冲击下多层机织织物的多尺度有限元建模
机译:凯夫拉尔纤维/碳纤维/玻璃纤维织物增强的混合复合层压板用于弹道冲击测试
机译:STF浸渍多层织物的弹道性能和行为的数值分析
机译:pBO和Kevlar织物的高温弹道冲击试验在超音速喷气发动机风扇密封系统中的应用