《第四届喷气推进与动力工程国际会议论文集》编著者第四届喷气推进与动力工程国际会议科学委员会、组织委员会。

为促进学科发展、国际交流合作以及人才培养，我院将于2012年9月10日～12日在西安举办第四届喷气推进与动力工程国际会议(4th ISJPPE)。会议由我院主办，北航、南航和德国亚琛工业大学(RWTH Aachen University)协办。其主要目的是总结或回顾近年来喷气推进与动力工程领域取得的主要进展，促进领域内学者和专家之间广泛交流，使之成为国内外科技人员激情创新、合作奋进的舞台。会议交流使用的正式语言为英语。

Session A:Turbomachinery, Internal Flow and Acoustics

The Numerical Simulation of Sand Trajectory in Fan Air Flow Channel of Turbo-fan Engine

Effects of Adverse Pressure Gradient on the Maximum Values of Reynolds Stresses in a Turbulent Boundary Layer 

Prediction and Analysis of Distortion Inlet on Compressor Performance and Stability Using Three Dimensional Model

Numerical Investigations on the Leakage Flow and Rotordynamic Characteristics of Labyrinth Seal

Study of Small Flow Rate High Pressure Ratio Backswept Impeller Design

A Model for Concentrated Vortices and an Unsteady Wake Model for Turbine

Study on Counter-Flow Thrust Vecotring Nozzle Jet Attachment and Control

Numerical Study of Cascade Self Noise WANG Liang-feng, QIAO Wei-Yang (65)

The Influence of Axial Turbine Element Stage Stator/Rotor Axial Spacing on Flow Status and Performance 

Experimental Investigation of Novel Casing Treatment with Bias Flow

Application and Optimization of Non-Axisymmetric End Wall in a High Pressure Turbine

Minimizing Secondary Flow Losses in a High Pressure Turbine with Nonaxisymmetric Endwall

Theoretical and Numerical Investigation of the Hydrodynamic Stability of the Planar Taylor-Culick Flow

Experimental Investigation of Axial Velocity Density Ratio in Large Camber Compressor Cascade                         

Optimization of Multi-Stage Axial Compressor Based on Stochastic Ranking DifferentialEvolution Algorithm

PIV Investigation of Secondary Flows in a Low-Speed Axial Compressor Rotor Passage                                                

Performance Improvement of a Degraded Heavy Duty Gas Turbine Using CFD Design Tools Research of Coaxial Gas Ejector

Numerical Research of the Best Depth and Location of the Circumferential Groove of Subsonic Compressor

Numerical Simulation of Turbine Performance with Low Reynolds Number at High Altitude              

Numerical Simulation of Three-Dimensional Separated Flow in a Linear Compressor Cascade

A Numerical Study of Active Flow Control for Low Pressure Turbine Blades

Influence of Turbulence Modeling on the Secondary Flow Predicition                         

2D Euler-Based Inverse Method. Development, Verification and Application

Session B：Heat and Mass Transfer

Session C：Muitiphase Flows,Reacting Flows and Combustion

Session D：Advanced Meaterials,Structural Strength, Vibration and Reliability

Session E：Propulsion Engine Design,Control and Health Management

Session F：Other Topics Relsted to Jet Propulsion and Power Engineering