机译:AP / HTPB复合推进剂对火箭发动机声振动的瞬态燃烧响应
Department of Mechanical and Nuclear Engineering. The Pennsylvania State University, University Park, Pennsylvania, USA;
Department of Mechanical and Nuclear Engineering. The Pennsylvania State University, University Park, Pennsylvania, USA;
Department of Mechanical and Nuclear Engineering. The Pennsylvania State University, University Park, Pennsylvania, USA;
AP/HTBP composite propellant; combustion instability; solid rocket motor; transient combustion;
机译:火箭发动机环境中Ap / htpb复合推进剂燃烧的模型
机译:基于多层夹心模型的非定常火箭发动机中AP / HTPB复合推进剂的火焰动力学
机译:基于多层夹心模型的非稳态火箭电机中AP / HTPB复合推进剂的火焰动态
机译:均质固体推进剂对火箭发动机声振荡的瞬时燃烧响应
机译:AP / HTPB复合推进剂在具有声振荡的火箭发动机中的两相流相互作用和燃烧。
机译:单分散高能释放核/壳结构铝纳米粉的制备及其在HTPB推进剂中作为助燃剂的应用
机译:轴对称火箭发动机中均质推进剂对声振荡的瞬态燃烧响应
机译:Vidhaeftning foer en HTpB-Baserad Kompositkrutisolering mot Nagra moderna Rakethylsmaterial(基于HTpB的复合推进剂衬里与现代火箭发动机外壳材料的粘合)