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《JOURNAL OF BALLISTICS》 1995-04
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THE NUMERICAL SIMULATION OF ROCKET GAS EFFLUN FIELD WITH FINITE-RATE CHEMICAL REACTION

Li Jun;Zhang Fuxing;Cao Congyong;Yang Yong(Mech.College.NUST,Nanjing,210094)  
In this thesis,the TVD Numerical Scheme suitable for nultiple species,finite-rate chemical reactine fluid has been deduced.It has been numerically cimulatecl for gas efflwo ofield of flying rocket.
【CateGory Index】: V430
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