J-GLOBAL ID:200904092342683445  Research Project code:9800036310 Update date:Dec. 11, 2001

Examination on aerodynamic phenomena with FITH of M-V rocket

Study period:1994 - 1999
Organization (1):
Investigating Researcher (3):
Research overview:
This study experimentally analyzes the mechanism of the interference between the rocket nozzle flow and the lower-stage rocket of FITH applied to the M-V rocket. Through the experiment, unsteady flow vibration due to that interference was found. Relation to its non-uniform separation phenomenon was found by numerical analysis.
Keywords (6):
launch ,  nozzle ,  gas ,  aerodynamic ,  flow ,  asymmetry
Research program: Ordinary Research
Ministry with control over the research :
Ministry of Education, Culture, Sports, Science and Technology

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