학위논문(박사) - 한국과학기술원 : 항공우주공학과, 2018.8,[viii, 75 p. :]
부분 분사▼a원형 노즐▼a초음속 충동형 터빈▼a반경 방향 힘▼a진동; partial admission▼acircular nozzle▼asupersonic impulse turbine▼aradial force▼avibration
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