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  • 2000,Vol 21,No. 2

    15 February 2000

Aerodynamic design system adapting to three dimensional turbine

2000, 21 (2): 1-4   

External reseach on flowfield of missile with direct lateral force control

2000, 21 (2): 5-7   

Aerothermodynamic numerical simulation of integrated small turbofan engine system

2000, 21 (2): 8-11   

Numerical simulation on post-stall behavior of turbofan engine

2000, 21 (2): 12-14   

Simulation of atomic radiation for plume spectrometry

2000, 21 (2): 15-18   

Numerical simulation of flow separation in nozzle

2000, 21 (2): 19-21   

Effects of axis acceleration load on forward dome insulation erosion for solid rocket motors

2000, 21 (2): 22-24   

Dynamic characteristics of priming process in spacecraft propulsion system (Ⅰ)theoretical model and simulation results

2000, 21 (2): 25-28   

Numerical simulation on viscous flow in the secondary flow path of a turbine sealed cabin

2000, 21 (2): 29-32   

Aerodynamic effect of trailing edge coolant ejection on transonic turbine cascade

2000, 21 (2): 33-36   

Nonlinear dynamics of shrouded-blades in contacting state

2000, 21 (2): 37-40   

Quadratic stability margin for systems with structured perturbations based on LMI

2000, 21 (2): 41-44   

LMI-based observer design for uncertain linear systems

2000, 21 (2): 45-47   

Experimental study of small perturbation induced rotating stall in axial flow compressor

2000, 21 (2): 48-51   

Critical rotational speed of turbo pump rotor (Ⅳ)transfer matrix method for the distributed mass shaft

2000, 21 (2): 52-55   

Numerical simulation on flowfield in supersonic combustor with cavity

2000, 21 (2): 56-59   

Numerical simulation on supersonic combustion of fuel-rich hot gas

2000, 21 (2): 60-63   

Nitrate ester plasticized thermoplastic polyurethane elastomers propellant

2000, 21 (2): 64-67   

Burning rate optimization of nitramine modified double base propellants with secondary flame inhibitors

2000, 21 (2): 68-71   

Influence of C60 ,fullerene soot and carbon black on combustion properties of catalyzed RDX-CMDB propellants

2000, 21 (2): 72-76   

Evaporation characteristic of N2O4/UDMH propellant in the air

2000, 21 (2): 77-80   

Azide polyurethane elastomer (Ⅰ)effect of intermolecular force on mechanical properties

2000, 21 (2): 81-83   

Relationship between gel decomposition characteristics and aging properties of HTPB propellants

2000, 21 (2): 84-87