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  • 1999,Vol 20,No. 6

    15 June 1999

USEFUL LIFE ASSESSMENT FOR A TYPE OF TURBOJET ENGINE

1999, 20 (6): 1-5   

PARITY SPACE METHOD FOR FAULT DIAGNOSIS OF LIQUID ROCKET ENGINE

1999, 20 (6): 6-9   

REAL-TIME SYSTEM FOR CONDITION MONITORING OF PROPULSION SYSTEM USING BP-ART HYBRID NEURAL NETWORKS

1999, 20 (6): 10-15   

PARALLEL SIMPLE ALGORITHM FOR COMPLEX FLOW SIMULATION IN LIQUID ROCKET ENGINE CHAMBER

1999, 20 (6): 16-18   

MODELING METHODS OF ACOUSTIC CAVITY IN COMBUSTION CHAMBER OF LIQUID ROCKET ENGINE

1999, 20 (6): 19-22   

NUMERICAL SIMULATION OF TURBULENT FLOW IN THE COMBUSTION CHAMBER OF A SPINNING SOLID ROCKET MOTOR

1999, 20 (6): 23-27   

FINITE ELEMENT ANALYSIS ON STRUCTURE STRENGTH OF A SOLID IMPULSIVE MICROTHRUSTER

1999, 20 (6): 28-31   

CALCULATION OF PHYSICS PERFORMANCE PARAMETERS OF INTERNAL FLOW FLUID FOR SFRJ

1999, 20 (6): 32-35   

NUMERICAL SIMULATION AND ANALYSIS OF REATTACHMENT POINT FOR SFRJ

1999, 20 (6): 36-39   

NUMERICAL SIMULATION OF FLOW SEPARATION IN NOZZLE

1999, 20 (6): 40-44   

STUDY OF SEAL RING OF TURBOJET ENGINE

1999, 20 (6): 45-47   

EXPERIMENTAL STUDY OF SMALL CALIBER ELECTROTHERMAL CHEMICAL HYPER VELOCITY LAUNCHING

1999, 20 (6): 48-51   

NUMERICAL SIMULATION ON THE INTERNAL PLASMA FLOW OF A SUPERSONIC ARCJET

1999, 20 (6): 52-57   

COMPUTER AIDED ROUTING SYSTEM FOR 3-D AIRCRAFT ENGINE PIPE

1999, 20 (6): 58-61   

PREDICTING TRANSIENT RESPONSE OF AXIAL COMPRESSORS TO PLANAR WAVE PRESSURE DISTURBANCE

1999, 20 (6): 62-65   

TIME MARCHING ALGORITHMS FOR SOLVING INCOMPRESSIBLE INTERNAL FLOW FIELD OF TURBOMACHINERY

1999, 20 (6): 66-69   

SIMULATION OF INTEGRATED PERFORMANCE OF AEROSPACE PLANE/AIR BREATHING PROPULSION SYSTEM

1999, 20 (6): 70-74   

INVESTIGATION OF SUPERSONIC COMBUSTION OF HYDROCARBON FUEL RICHED HOT GAS

1999, 20 (6): 75-79   

ANALYSIS OF EROSION AT THE SLOTTED TUBE EXIT SURFACES OF A HOT GAS GENERATOR

1999, 20 (6): 80-83   

EXPERIMENTAL STUDY ON DISTRIBUTION PATTERN OF PARTICLES IN SRM NOZZLE

1999, 20 (6): 84-86   

EXPERIMETNAL STUDY ON THE COMBUSTION PHENOMENON OF CATALYSED MODIFIED SOLID PROPELLANTS

1999, 20 (6): 87-91   

STUDY OF COMBUSTION WAVE TEMPERATURE DISTRIBUTION OF GAP/AN PROPELLANT

1999, 20 (6): 92-95   

MICROMECHANICS ANALYSIS ON THE VISCOELASTICS CONSTITUTIVE LAW OF COMPOSITE SOILD PROPELLENT (Ⅰ)REINFORCEMENT EFFECT OF BALL PARTICULATES

1999, 20 (6): 96-99   

STABILIZATION OF POLYETHER URETHANE BINDER IN SOLID PROPELLANT

1999, 20 (6): 100-105   

ICT SCAN SYSTEM FOR SOLID ROCKET MOTORS

1999, 20 (6): 106-108   

STRENGTH FORMULA OF PROPELLANT SAFETY IMPACT WITH RELIABILITY LEVEL

1999, 20 (6): 109-112