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S0510502 Control of Mach wave emission angle using helical modes in a supersonic jet
S0510502 ヘリカルモードを用いた超音速ジェットのマッハ波放射方向制御([S051-05]噴流,後流およびはく離流れ現象の探求と先端的応用(5))
2014
The Proceedings of Mechanical Engineering Congress Japan
S0510502 ヘリカルモードを用いた超音速ジェットのマッハ波放射方向制御([S051-05]噴流,後流およびはく離流れ現象の探求と先端的応用(5))
Preserved Fulltext
The three − dimensional time dependent compressible Navier − Stokes equations are numerically solved to study acoustic emission nature in a supersonic round jet at high convective Mach number ( M ← 2. 0 ) using high − order compact upwind schemes
doi:10.1299/jsmemecj.2014._s0510502-
fatcat:6oi4ymwfkvbs7ow5vlbj7s23ku