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Current Issue

Structure, Strength and Reliablity

Simulation Analysis on the Opening Process and Movement of Pulse Separation Device in Dual Pulse Motor

LE Hao1, 覃海艺2,3, 崔振山

2020, 41 (7): 0-   

The Numerical Analysis of Potential Drop Test on Micro-notched Specimen

2020, 41 (7): 0-   

The validation and application of over-speed analysis using strain-based fracture criteria

WANG Kaiming1,2

2020, 41 (7): 0-   

Material,Propellant and Fuel

Research on dynamic impact damage of HTPB propellant under different states

Chen Xiang-dong

2020, 41 (7): 0-   

System

Numerical investigations about running characteristics of hypersonic wind tunnel

CONG Cheng-hua

2020, 41 (7): 0-   

Aero-thermodynamics

Application of Loss and Deviation Surrogate Model in Prediction of Multistage Axial Compressor Characteristics

Han Changfu

2020, 41 (7): 0-   

Research on Applications of Scale-Adaptive Simulation in Transonic Turbine

WANG Guo-liang

2020, 41 (7): 0-   

Combustion , Heat and Mass Transfer

Study on the Breaking Process of Liquid Jet in Supersonic Flow Based on Adaptive Mesh

2020, 41 (7): 0-   

Flow and Heat Transfer Investigation on Compound Cooling of Liquid Rocket Engine Thrust Chamber

YANG Cheng-xiao, 王长辉

2020, 41 (7): 0-   

Test,Experiment and Control

High-order Modal Shape Measurement of Centrifugal Impeller Blade by Using Marco Fiber Composite

2020, 41 (7): 0-   

Combustion , Heat and Mass Transfer

Simulation on swirl liquid sheet spray process based on moving particle Semi-implicit method

2020, 41 (7): 0-   

Aero-thermodynamics

Numerical Investigation on Effects of Installation Height of Fins on Drag Reduction Performance of Co-rotating Cavity

HOU Xiao-ting

2020, 41 (7): 0-   

Test,Experiment and Control

Research on Inlet and Engine integrated model stability control Based on Auxiliary door

YE Dong-xin

2020, 41 (7): 0-   

Combustion , Heat and Mass Transfer

Study on the Mechanism of Pre-mixed CH4-O2 Mixture Detonation Propagation in the Annular Channel

2020, 41 (7): 0-   

Test,Experiment and Control

Performance Seeking Control of Turbofan Engine Minimum Fuel Consumption Model Based on GA-SQP

liyong

2020, 41 (7): 0-   

Structure, Strength and Reliablity

Research on Aero-Gear Pump Journal bearings Start-up Transient lubrication characteristics with radial micro-motion analysis coupled CFD

ZHU Jia-xing1,2, 魏士杰, 刘显为

2020, 41 (7): 0-   

Combustion , Heat and Mass Transfer

Effect of Film Hole Row Location on Film Cooling Characteristic on the Pressure Side of a Turbine Vane

YAO Chun-yi

2020, 41 (7): 0-   

Ship Propulsion

Research on Optimization Effect of the Modified Conformal Rudder with a Flat Part on Submarine Wake Field

Zhai Shuo

2020, 41 (7): 0-   

Combustion , Heat and Mass Transfer

Comparative Analysis of Flow between Tube Typed and Cascade Typed De-Swirl Nozzles

HAO Yuan-hui

2020, 41 (7): 0-   

Numerical Investigation of Flow and Volume Flow Rate Characteristics of Oil Jet Nozzles with Two Orifices

JIANG Le

2020, 41 (7): 0-   

Experimental Study on Characteristics of DC Gliding Arc Plasma Igniter

2020, 41 (7): 0-   

Aero-thermodynamics

Effects of Surface Roughness on the Aerodynamic Performance of a High Subsonic Compressor Airfoil Under Low Reynolds Number Conditions

wangmingyang

2020, 41 (7): 0-   

Design and Investigation of Blade Tip Winglet for TransonicFan Rotor

2020, 41 (7): 0-   

Study on the characteristics of high Mach number inward turning inlet under real gas effect

2020, 41 (7): 0-   

Electric Propulsion and Other Advanced Propulsion

Experimental Investigation of Nacelle Inlet Crosswind Flow Separation Control by Microsecond Pulsed Dielectric Barrier Discharge Plasma

HE Qi-kun

2020, 41 (7): 0-   

System

The effect of radial distribution of core driven fan stage aerodynamic parameters on variable cycle engine performance

SONG Fu1,2

2020, 41 (7): 0-   

Combustion , Heat and Mass Transfer

Investigation on Schemes for Accelerating Oxidizer Boost Pump during Start-up of LOX/kerosene Staged Combustion Rocket Engine

WANG Chun-min1

2020, 41 (7): 0-