An experimental and computational study on self-excited oscillations in supersonic opposing jet flows

Transactions of the Japan Society for Aeronautical and Space Sciences

Volumn 42, Issue 137, 1999, Pages 112-119

  Fujita, Masahiro ^a   Karashima, Keiichi ^b  

^a MITSUBISHI RESEARCH INSTITUTE   (Japan)

^b NISHINIPPON INSTITUTE OF TECHNOLOGY   (Japan)

Author keywords

Axisymmetric Flow Model; Jet Structure; Recirculating Region; Unsteady Flow

Indexed keywords

ALGORITHMS; COMPRESSIBLE FLOW; COMPUTER SIMULATION; FINITE DIFFERENCE METHOD; FLOW VISUALIZATION; JETS; MATHEMATICAL MODELS; OSCILLATIONS; PRESSURE TRANSDUCERS; UNSTEADY FLOW; VISCOUS FLOW; WIND TUNNELS;

MACH NUMBER; SUPERSONIC OPPOSING JET FLOW;

SUPERSONIC FLOW;

EID: 0033226074     PISSN: 05493811     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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