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Current Issue

  • 1988,Vol 9,No. 6

    15 June 1988

AN INTEGRATED METHOD FOR CALCULATING UNIFIED FLOWFIELD IN SOLID ROCKET MOTOR

1988, 9 (6): 1-9   

A TEST STUDY OF THE VARIABLE-THRUST LIQUID ROCKET ENGINE

1988, 9 (6): 10-13   

A THEORITICAL CALCULATION OF GAS TURBULENT RECIRCULATION FLOW IN THE COMBUSTION CHAMBER OF ROCKET ENGINE

1988, 9 (6): 14-17   

THE TEMPERATURE PREDICTION FOR COMPOSITE NOZZLE OF SOLID ROCKET MOTOR UNDER ABLATION

1988, 9 (6): 18-23   

EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER CONTROL OF TWO-DIMENSIONAL CONVERGENT-DIVERGENT DUCT WITH TERMINAL TRANSONIC SHOCK-WAVE

1988, 9 (6): 24-30   

A HIGH SPEED PHOTOGRAPHIC STUDY OF FLUID TRANSIENTS IN TURBOPUMP FUEL SYSTEM

1988, 9 (6): 31-36   

A METHOD FOR CONVERTING GROUND TEST RESULTS TO VACUUM PARAMTERS OF SPACE ROCKTS

1988, 9 (6): 37-40   

EXPERIMENTAL INVESTIGATION OF CRACK GROWTH IN SOLID PROPELLANTS

1988, 9 (6): 41-47   

THE EFFECTS OF RDX/AP PROPORTION ON HTPB COMPOSITE PROPELLANT COMBUSTION PROPERIES AT LOW PRESSURE

1988, 9 (6): 48-53   

PROPELLANT MANAGEMENT FOR SATELLITE PROPULSION SYSTEM UNDER MICROGRAVITY

1988, 9 (6): 54-58