24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-3.4.3

MACH WAVE EMISSION IN A PLANE SUPERSONIC JET AT HIGH CONVECTIVE MACH NUMBERS
D. Watanabe , H. Maekawa
Graduate School of Engineering, Hiroshima University, Japan
Keywords: Supersonic jet, Transition, Turbulence, Mach wave, DNS

The three-dimensional time dependent compressible Navier-Stokes equations are numerically solved to study acoustic emission mechanism in a supersonic plane jet at high convective Mach numbers using high-order compact upwind schemes.

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24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan Paper ICAS 2004-3.4.3

MACH WAVE EMISSION IN A PLANE SUPERSONIC JET AT HIGH CONVECTIVE MACH NUMBERS

D. Watanabe , H. Maekawa Graduate School of Engineering, Hiroshima University, Japan

Keywords: Supersonic jet, Transition, Turbulence, Mach wave, DNS The three-dimensional time dependent compressible Navier-Stokes equations are numerically solved to study acoustic emission mechanism in a supersonic plane jet at high convective Mach numbers using high-order compact upwind schemes.

view full paper

24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-3.4.3

D. Watanabe , H. Maekawa
Graduate School of Engineering, Hiroshima University, Japan

Keywords: Supersonic jet, Transition, Turbulence, Mach wave, DNS

The three-dimensional time dependent compressible Navier-Stokes equations are numerically solved to study acoustic emission mechanism in a supersonic plane jet at high convective Mach numbers using high-order compact upwind schemes.