High-aspect-ratio cooling channel concept tested in Lewis' rocket engine test facility

被引:0
|
作者
机构
来源
NASA Tech Memo | / 107111卷 / 83期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 31 条
  • [31] Effects of gaps between the side-walls and ribs on the rib-induced flow structure and heat transfer distribution inside a high aspect ratio cooling channel
    Kiml, R.
    Mochizuki, S.
    Murata, A.
    Journal of Flow Visualization and Image Processing, 2002, 9 (2-3) : 211 - 228