...
机译:MACH编号2.5扁平钝板边界层弱冲击波影响的实验研究
Russian Acad Sci Siberian Branch Khristianovich Inst Theoret &
Appl Mech Inst Skaya Ul 4-1 Novosibirsk 630090 Russia;
Russian Acad Sci Siberian Branch Khristianovich Inst Theoret &
Appl Mech Inst Skaya Ul 4-1 Novosibirsk 630090 Russia;
Russian Acad Sci Siberian Branch Khristianovich Inst Theoret &
Appl Mech Inst Skaya Ul 4-1 Novosibirsk 630090 Russia;
Russian Acad Sci Siberian Branch Khristianovich Inst Theoret &
Appl Mech Inst Skaya Ul 4-1 Novosibirsk 630090 Russia;
Russian Acad Sci Siberian Branch Khristianovich Inst Theoret &
Appl Mech Inst Skaya Ul 4-1 Novosibirsk 630090 Russia;
supersonic flow; N-wave; turbulence; experiment; boundary layer; hot-wire anemometry;
机译:MACH编号2.5扁平钝板边界层弱冲击波影响的实验研究
机译:激波与钝板和钝板边界层的相互作用
机译:弱电离流对钝体周围冲击层电磁影响的实验研究
机译:几个弱冲击波对钝平板边界层影响的实验研究
机译:通过环形管道(SCRAMJET)进行超音速流场中冲击波和湍流边界层相互作用的实验研究。
机译:纳米流体的mHD自由对流边界层流过一垂直平板与牛顿暖气边界条件
机译:在Mach编号2.5中板边界层对弱冲击波动作的实验研究
机译:用平板和湍流边界层分析平板边界层的弱冲击波反射I-ITERaCTION用层次和湍流边界层分析的动量积分法