24th Congress of International Council of the Aeronautical Sciences, 29 August-3, September 2004, Yokohama, Japan
Paper ICAS 2004-3.6.4

NUMERICAL SIMULATION OF SUPERSONIC FLOWFIELD WITH SECONDARY INJECTION

R. S. Amano, D. Sun
University of Wisconsin-Milwaukee, USA

Keywords: shock wave, supersonic flow, jet injection

Two and three-dimensional steady flowfields generated by transverse secondary injection into a supersonic flow, was simulated by solving the Favre-averaged Navier-Stokes equations using the weighted essentially nonoscillatory (WENO) schemes and the Jones-Launder k-e model. Both the two-dimensional and three dimensional results are given.

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