最近搜尋
    大家都在找

        An Experimental Investigation by Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8.

        NTD699

        金石堂

        前往賣場
        An Experimental Investigation by Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8.
          1. An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8.

            An Experimental Investigation of Hypersonic Flow Over Blunt Nosed Cones at a Mach Number of 5.8.

            NTD699
            金石堂
          1. An Experimental Investigation of Flow Over Simple Blunt Bodies at a Mach Number of 5.8.

            An Experimental Investigation of Flow Over Simple Blunt Bodies at a Mach Number of 5.8.

            NTD753
            金石堂