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Current Issue

  • 1999,Vol 20,No. 2

    15 February 1999

NEURAL NETWORK APPROACH TO FAULT DETECTION OF LIQUID ROCKET ENGINE (Ⅱ)PATTERN RECOGNITION TECHNOLOGY

1999, 20 (2): 1-4   

NUMERICAL ANALYSIS OF ACOUSTICAL WAVE MOTION IN COMBUSTION CHAMBER OF LIQUID ROCKET ENGINE

1999, 20 (2): 5-8   

ADVANCED MODEL OF STATIC CHARACTERISTIC FOR LIQUID OXYGEN/KEROSENE PROPELLANT STAGED COMBUSTION ROCKET ENGINE

1999, 20 (2): 9-12   

EFFECT OF THRUST BIAS AND GRAIN INITIAL TEMPERATURE ON RANGE AND CROSSWISE DEVIATION OF SPINNING ROCKET

1999, 20 (2): 13-16   

OPTIMAL DESIGN OF ACCELERATING CONTROL LAW FOR VARIABLE GEOMETRY TURBOFAN ENGINE

1999, 20 (2): 17-20   

STUDY ON STARTUP MODEL AND STARTUP CONTROL LAW OF TURBOFAN ENGINE

1999, 20 (2): 21-24   

STORAGE AND RESTORATION OF STANDARD SIGNAL OF AERIAL ENGINE

1999, 20 (2): 25-27   

NUMERICAL SIMULATION STUDY OF SCRAMJET FLOW FIELD

1999, 20 (2): 28-32   

MECHANICS ANALYSIS ON THE SPATIAL MECHANISM OF DOUBLE EXTENDIBLE NOZZLE

1999, 20 (2): 33-36   

NUMERICAL SIMULATION OF TWO DIMENSIONAL TRANSONIC TWO PHASE TURBULENT FLOW IN NOZZLE

1999, 20 (2): 37-41   

STUDY ON CRITICAL ROTATIONAL SPEED OF TURBOPUMP ROTORS(Ⅲ)FOR TURBOPUMP ROTORS TAKING ACCOUNT OF LIQUID ACTING FORCES

1999, 20 (2): 42-44   

FUZZY RELIABILITY DESIGN AND ESTIMATION METHOD FOR LONG LIFE SPAN TURBOPUMP

1999, 20 (2): 45-48   

NUMERICAL SIMULATIONS OF MIXING ENHANCEMENT OF RAMP INJECTORS IN SCRAMJET COMBUSTOR

1999, 20 (2): 49-52   

3D NUMERICAL SIMULATION OF HYPERSONIC JET INTERACTION FLOWFIELD

1999, 20 (2): 53-55   

ON MODEL OF STAGE BY STAGE DYNAMIC BLADE RESPONSE FOR PREDICTING AERODYNAMIC STABILITIES IN MULTISTAGE AXIAL COMPRESSORS WITH INLET DISTORTIONS

1999, 20 (2): 56-60   

SIMULATION ON FLOW AND MIXING OF TURBULENT IN DIVERGING DUCT

1999, 20 (2): 61-63   

EXPERIMENTAL INVESTIGATION OF FILM COOLING HEAT TRANSFER ON TURBINE BLADE LEADING EDGE

1999, 20 (2): 64-68   

NUMERICAL SIMULATION ON ANGLE FACTOR OF OUTWARD RADIATION FOR FOUR DIAGONALLY ARRANGED NOZZLES

1999, 20 (2): 69-72   

SPRAY PROPERTY RESEARCH AND APPLICATION OF UNLIKE IMPINGING INJECTOR

1999, 20 (2): 73-76   

STUDY ON BURNING RATE CONTROL OF LOW BURNING RATE HTPB PROPELLANT

1999, 20 (2): 77-82   

NITROGEN OXIDES POTENTIAL OXIDANT OF ALUMINUM

1999, 20 (2): 83-87   

EFFECT OF PROPELLANT COMPONENTS ON DEGRADATION OF POLYETHER URETHANE BINDER (Ⅰ)THE EFFECT OF NITRATE ESTERS

1999, 20 (2): 88-94   

FLAMMABILITY LIMITS OF ALUMINUM MAGNESIUM FUEL RICH PROPELLANT

1999, 20 (2): 95-98   

ANALYSIS OF SOLID PROPELLANT CONTROL THRUSTER SCHEMES FOR SMALL KKV

1999, 20 (2): 99-102   

REVIEW OF AIRFRAME/INLET INTEGRATION OF MANEUVER FIGHTER AIRCRAFT

1999, 20 (2): 103-107   

SUMMARY OF TYPIC LABORATORY AND TEST ABOUT LIQUID ROCKET ENGINE

1999, 20 (2): 108-112