25th Congress of International Council of the Aeronautical Sciences, 3 - 8 September 2006, Hamburg, Germany
Paper ICAS2006-2.2S
NUMERICAL SIMULATION OF THE FLOWFIELD AROUND MISSILE WITH LATERAL JET INTERACTION
D. Sun, X. Jia, X. Liang
Northwestern Polytechnical Univ., China
Keywords: Jet Interaction, Air-to-Air Missile, Endgame, Numerical Simulation
A third order Weight ENO scheme was used to simulate the interaction flowfield around a slender body and a missile with fins. The parameters that influence the flowfield and the transient startup phase were studied in detail for both cases. The results are useful to missile autopilot design.
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