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Current Issue

Development and Application of Hybrid Rocket Motor Technology:Overview and Prospect

2012, 33 (6): 831-839   

A Model Based on Lumped Parameter Method for Scramjet Performance Computation

2012, 33 (6): 840-846   

Model-Based Research on Matching Exhaust Turbocharger and Engine

2012, 33 (6): 847-852   

Combustion , Heat and Mass Transfer

Experimental Investigation on Boundary Layer Suction in a Highly-Loaded Compressor Cascade

2012, 33 (6): 853-858   

Measurement of the Transition and Separation for Turbine Blade Boundary Layer with Low-Reynolds Number

2012, 33 (6): 859-865   

Research on Dynamic Characteristics for a Super-High Speed Rotor System II:Rotor System with Rubs

2012, 33 (6): 866-874   

Experimental Investigations on the Discharge Coefficient of Double-DeckerJet Impingement/Film Structures

2012, 33 (6): 875-880   

Effects of Rotational Speed Ratio on Stability Boundary of Contra-Rotating Compressor

2012, 33 (6): 881-887   

Investigation on Multi-Stage Turbine Aerodynamic Design and Optimization

2012, 33 (6): 888-896   

Experimental Investigation on Catalytic Hydrogen and Oxygen Thruster

2012, 33 (6): 897-901   

Effects of Temperature and Pressure on Pressure Oscillation in the Chamber of Solid Rocket Motor

2012, 33 (6): 902-906   

Study on Mixing and Combustion of Kerosene Fuel in Ramjet Mode of RBCC Engine

2012, 33 (6): 907-913   

Kinetic Simulation of Combustion Process in Individual Flame Tube

2012, 33 (6): 914-922   

Experimental Investigation of Supersonic Combustion Flame Structure with Strut Injectors

2012, 33 (6): 923-927   

Effects of Injectors Locations on Kerosene Combustion in Supersonic Combustor

2012, 33 (6): 928-933   

Phenomenon of Phase Separation in Combustion Process of Organic Gelled Fuel Droplets

2012, 33 (6): 934-939   

Experimental and Numerical Study of the Truncated SERN

2012, 33 (6): 940-945   

Studies on Control Method of Two Dimensional Fluidic Throat Skewing Vectoring Nozzle

2012, 33 (6): 946-950   

Design of Nonlinearly Compressed SERN Profile

2012, 33 (6): 951-955   

Experimental Study on Vortex-Cooled Thrust Chamber

2012, 33 (6): 956-960   

Aero-Engine Fault Diagnosis by a New Fast Multi-Class Support Vector Algorithm

2012, 33 (6): 961-967   

Controller Design Methodology for Aeroengine Nozzle with Actuator

2012, 33 (6): 968-973   

Application of Particle Swarm Optimization in Obtaining Solution of Aeroengine Component-Level Model

2012, 33 (6): 974-980   

Numerical Modeling and Simulation of Turbine Test Rig Combustion Device()Partition Model Based on Mixture Fraction

2012, 33 (6): 981-986   

Investigation on Performance of Small-Thrust Bi-Propellant Thruster for Attitude Control

2012, 33 (6): 987-990   

Numerical Analysis for Electron Backstreaming Accelerator Grid Limited Voltage for 20cm Xe Ion Thruster Grid System

2012, 33 (6): 991-996