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《第4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（4thISJPPE）。会议由我院主办，北航、南航和德国亚琛工业大学（RWTHAachenUniversity）协办。

内容简介

　　本书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。

目　　录

Contents
Session A.Turbomachinery,Internal Flow and Acoustics
The Numerical Simulation of Sand Trajectory in Fan Air Flow Channelof Turbo-fan Engine
Effects of Adverse Pressure Gradient on the Maximum Values ofReynolds Stresses in a
Turbulent Boundary Layer MA Wei,Ottavy Xavier,LU Li-peng,LeboeufFrancis (24)
Prediction and Analysis of Distortion Inlet on CompressorPerformance and Stability Using Three Dimensional Model
Numerical Investigations on the Leakage Flow and RotordynamicCharacteristics of Labyrinth Seal
Study of Small Flow Rate High Pressure Ratio Backswept ImpellerDesign
A Model for Concentrated Vortices and an Unsteady Wake Model forTurbine
Study on Counter-Flow Thrust Vecotring Nozzle Jet Attachment andControl
Numerical Study of Cascade Self Noise
The Influence of Axial Turbine Element Stage Stator/Rotor AxialSpacing on Flow Status and Performance
Experimental Investigation of Novel Casing Treatment with BiasFlow
Application and Optimization of Non-Axisymmetric End Wall in a HighPressure Turbine

Contents 
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 MA Wei,Ottavy Xavier,LU Li-peng,Leboeuf
Francis (24) 
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 
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 Differential Evolution 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 
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 
20 Years of Experiences f0r the Conjugate Heat Transfer Analysis 0f
Convection-cooled Turbine Vanes 
Industrial Applications of Heat Transfer Enhancement.Review and
Problem 
Heat Tranvafer Augmentation Technol Ogies for Internal Cooling of
Turbine Components of Gas Turbine Engines 
Thermodynamics Characteristic of the Flow and Heat Transfer in
Rotating Cavity 
…… 
Session C:Multiphase Flows,Reacting Flows and Combustion 
Session D:Advanced Materials,Structural Strength,Vibration and
Reliability 
Session E:Propulsion Engine Design,Control and Health
Management 
Session F:Other Topics Related to Jet Propulsion and Power
Engineering

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