NUMERICAL SIMULATION OF HEAT TRANSFER IN TRANSPIRATION COOLED LIQUID ROCKET THRUSTER CHAMBER(Ⅰ) PHYSICAL MATHEMATICAL MODEL

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1999, 20 (3)： 1-4   

START UP SIMULATION OF A LIQUID PROPELLANT STAGED COMBUSTION ROCKET ENGINE

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1999, 20 (3)： 5-9   

SENSITIVITY ANALYSIS OF SSTO VEHICLE PARAMETERS

Abstract ( ) PDF (684KB) ( )

1999, 20 (3)： 10-12   

STUDY OF DSMC METHOD FOR EXHAUST PLUME IMPINGEMENT EFFECTS ON SPACECRAFT SURFACES

Abstract ( ) PDF (1012KB) ( )

1999, 20 (3)： 13-16   

NUMERICAL STUDIES FOR INTERACTION FLOWFIELD BETWEEN SUPERSONIC FLOW AROUND BODY AND JET FLOW EXHAUSTING FROM ROCKET

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1999, 20 (3)： 17-20   

EXPERIMENTAL INVESTIGATION ON DETONATIVE RANGE,INNER FLOW GAS TEMPERATURE AND WALL TEMPERATURE OF PULSED DETONATION ENGINE

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1999, 20 (3)： 21-24   

STUDY ON ENGINE MILITARY REGIME CONTROL FOR ADVANCED FIGHTER

Abstract ( ) PDF (1023KB) ( )

1999, 20 (3)： 25-29   

EXPERIMENTAL STUDY OF ANOMALOUS COMBUSTION IN SOLID PROPELLANT GRAIN WITH DEFECTS

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1999, 20 (3)： 30-35   

NUMERICAL ANALYSIS OF CONVECTIVE BURNING FLOW FIELD IN PROPELLANT CRACK

Abstract ( ) PDF (856KB) ( )

1999, 20 (3)： 36-39   

INVESTIGATION OF SIDEWALL COMPRESSION INLET WITH CONSTANT PRESSURE RATION AND CURVED LEADING EDGE UNDER NONUNIFORM SUPERSONIC FLOW

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1999, 20 (3)： 40-44   

PARAMETERS IDENTIFICATION OF ALKALI METAL IMPURITIES OF SOLID PROPELLANT AND PROPERTIES OF EXHAUST AFTERBURNING

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1999, 20 (3)： 45-49   

TWO DIMENSIONAL AND TWO PHASE COLD FLOW TEST IN ENTRANCE REGION OF SUBMERGED NOZZLE

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1999, 20 (3)： 50-52   

STUDY ON STRUCTURAL AGEING RELIABILITY FOR FLEXIBLE JOINT OF SOLID ROCKET MOTOR

Abstract ( ) PDF (867KB) ( )

1999, 20 (3)： 53-55   

COMPUTATION OF DUAL MODE SUPERSONIC COMBUSTOR

Abstract ( ) PDF (1278KB) ( )

1999, 20 (3)： 56-60   

EXPERIMENT MODAL ANALYSIS ON FRONT BEARING SPRING SUPPORT FOR TURBOJET ENGINE

Abstract ( ) PDF (733KB) ( )

1999, 20 (3)： 61-63   

EFFECTS OF INLET FLOW CONDITIONS ON BOUNDARY FLOW ON COMPRESSOR BLADE SURFACE

Abstract ( ) PDF (1208KB) ( )

1999, 20 (3)： 64-68   

EXPERIMENT STUDY ON EFFECT OF TIP CLEARANCE ON CENTRIFUGAL IMPELLER PERFORMANCE

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1999, 20 (3)： 69-72   

SOLUTION OF PARAMETRIC RICCATI EQUATION ON TURBOJET ENGINE H ∞ CONTROL

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1999, 20 (3)： 73-77   

RESEARCH OF CAD TECHNOLOGY IN AEROENGINE DESIGN

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1999, 20 (3)： 78-80   

COMBUSTION PROPERTIES OF HTPB PROPELLANTS WITH BURNING RATE CATALYSTS AT HIGH PRESSURE

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1999, 20 (3)： 81-85   

STUDY ON THERMAL DECOMPOSITION CHARACTERISTICS OF GAP/AN PROPELLANT

Abstract ( ) PDF (1160KB) ( )

1999, 20 (3)： 86-90   

RELATIVITY STUDY ON PYROLYTIC CHARACTERISTICS AND CATALYTIC ACTIVITIES OF SOME NTO SALTS IN SOLID PROPELLANT

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1999, 20 (3)： 91-94   

EFFECT OF PROPELLANT COMPONENTS ON DEGRADATION OF POLYETHER URETHANE BINDER (Ⅱ)EFFECTS OF ENERGETIC FILLERS AND ADDITIVES

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1999, 20 (3)： 95-99   

STUDIES ON MORPHOLOGICAL STRUCTURE OF HIGHLY PLASTICIZED POLYETHYLENE GLYCOL POLYURETHANE ELASTOMER

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1999, 20 (3)： 100-102   

STUDY ON ZERO POINT VARIATION OF SOLID ROCKET ENGINE TESTING SYSTEM

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1999, 20 (3)： 103-106   

SURVEY OF INTERNAL PROCESS STUDIES ON ARCJET THRUSTERS

Abstract ( ) PDF (1638KB) ( )

1999, 20 (3)： 107-112