Proj
J-GLOBAL ID:200904051182838295  Research Project code:9800042438 Update date:Dec. 11, 1997

Study on numerical simulation of flow field on super sonic retro-firing jet

超音速逆噴射ジェットの流れ場の数値シミュレーション
Study period:1995 - 1996
Keywords (6):
supersonic ,  gas ,  flow ,  numerical ,  self-induced ,  axisymmetric
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

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