Transactions of Nanjing University of Aeronautics & Astronautics
Numerical Simulation of Transverse Jet Interaction with Rudders in Supersonic Free Stream for Simplified Missile
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Abstract:
Numerical simulation is carried out for jets arranged at 7 different positions for the same model and compared with non-jet flows. The total and rudder force and moment amplification is calculated and analyzed by the pressure distribution on the surface and rudders of the simplified missile. Numerical results show that interactions take great effect on the configuration of the flow field around rudders and the pressure distribution on the missile surface.
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Project Supported:
This work was supported in part by Fundamental of Graduate Innovation Center in NUAA (No. kfjj20170122) and the Fundamental Research Funds for the Central Universities.
Clc Number:
V21
CHINA AERO-SCIENCES
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