J-GLOBAL ID:200904030874254369  Research Project code:9950000135 Update date:Feb. 29, 2000

Experimental and analytical study on supersonic cavity flow

Study period:1997 - 1997
Organization (1):
Investigating Researcher (3):
Research overview:
This study deals with the cavity used to control the shock wave in the air intake port of supersonic or hypersonic aircraft.
Keywords (3):
超音速機 ,  衝撃波 ,  キャビティ
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

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