Proj
J-GLOBAL ID:200904023431885564  Research Project code:9800045499 Update date:Nov. 20, 2003

Study on elucidation of shock wave structure in super sonic jet and on exfoliation of turburant flow within boundary layer

超音速噴流中の衝撃波構造の解明,境界層内乱流の剥離に関する研究
Study period:1997 - 1997
Organization (1):
Investigating Researcher (1):
Keywords (7):
supersonic ,  jet(flow) ,  shock ,  structure ,  boundary ,  turbulent ,  exfoliation
Research program: Ordinary Research

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