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Current Issue

Aero-thermodynamics

Calculating Performance of Pulse Detonation Turbo Engine

2012, 33 (5): 665-670   

Ship Propulsion

Analysis on Boundary Layer Flow Stability of Hypersonic Wedge

2012, 33 (5): 671-675   

Experimental Investigation on the Shock Wave Oscillation Behaviors in a Two-Dimensional Hypersonic Inlet Flow

2012, 33 (5): 676-682   

Numerical Investigation of Effects of Cowl Lip Shape on 2-D Inlet

2012, 33 (5): 683-688   

Combustion , Heat and Mass Transfer

Design Optimization for a Transonic Compressor with Implementation of Non-axisymmetric Endwall Contouring

2012, 33 (5): 689-694   

Research on Dynamic Characteristics for a Super-High Speed Rotor System (I):Rotor System Without Rubs

2012, 33 (5): 695-703   

Numerical Simulation on the Effect of Film Cooling at Leading Edge of Turbine Blade with Two Rows of Staggered Holes

2012, 33 (5): 704-709   

Numerical Study on Impinging Cooling for a High-Pressure Turbine Blade

2012, 33 (5): 710-718   

Three-Dimensional Numerical Investigation on Aerodynamic Performance in a Supersonic Tandem Rotor

2012, 33 (5): 719-725   

Impact of Internal Combustion Wave Rotor on Performance of Turboshaft Engine

2012, 33 (5): 726-731   

Numerical Study of Pre-Swirl Flow in Rotating Cascade of a Small Gas Turbine

2012, 33 (5): 732-739   

Effects of Pre-Swirl Angle on Flow Characteristics of Pre-Swirl Nozzle

2012, 33 (5): 740-746   

Boundary Layer Passive Control of an Ultra-High-Lift Low-Pressure Turbine Blade

2012, 33 (5): 747-753   

Analysis on the Crystallographic Slip Constitutive Models for Single Crystal Turbine Blade

2012, 33 (5): 754-759   

Numerical Study of Co-Axial Pilot and Main Module Combustor

2012, 33 (5): 760-764   

Experimental Study on Atomization Characteristics of Liquid Injection in Simulated Space Environment

2012, 33 (5): 765-770   

Experimental Investigation on Spray Characteristics from Superheated Liquid Jets under Low Pressure

2012, 33 (5): 771-778   

Effect of Kerosene Distribution on Combustion Performance in Supersonic Combustor

2012, 33 (5): 779-784   

Analysis of Combustion Characteristics in the Region with Violent Pressure Oscillations in Thruster Chamber

2012, 33 (5): 785-789   

Numerical Analysis and Test on Work Process of Pulse Separation Device in Pulse Motor

2012, 33 (5): 790-794   

Material,Propellant and Fuel

Research on Hyperelastic Constitutive Model for HTPB Crosslinked Specimen

2012, 33 (5): 795-798   

Synthesis and Curing Research of Propargyl-Terminated PET

2012, 33 (5): 799-803   

Numerical Simulation of Fluid Transients by Chebyshev Super Spectral Viscosity Method for Propellant Lines

2012, 33 (5): 804-808   

Three Dimensional Thermomechanical Analysis of Liquid Rocket Engine Thrust Chamber Inner Wall

2012, 33 (5): 809-813   

Control ,Measurement and Fault Diagnosis

Research of the Flow Regulator Nonlinear Frequency Characteristics by Incremental Harmonic Balance Method

2012, 33 (5): 814-819   

New Propulsion System

Numerical Investigation for Rotating Detonation Engine

2012, 33 (5): 820-825   

Effect of Axial Position of Ejectors with Variable Cross-Section Area on Performance of a Pulse Detonation Rocket Engine

2012, 33 (5): 826-