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Current Issue

Aero-thermodynamics

Performance simulation of air-turbo-rocket with water injection pre-cooler

2011, 32 (1): 1-4   

Three-dimensional simulation of H2O vitiation effects on combustor performance for scramjet

2011, 32 (1): 5-10   

Characteristics of SteamJet with coolants/oxidizers

2011, 32 (1): 11-16   

Aero-engine performance calculation model based on a new algorithm of turbine cooling

2011, 32 (1): 17-20   

Equilibrium-manifold based linear parameter varyingmodeling for aeroengine

2011, 32 (1): 21-25   

Connected-pipe experiment and analysis for ducted rocket

2011, 32 (1): 26-31   

Life prediction of shipborne solid rocket motor under the ship swing motion

2011, 32 (1): 32-35   

Ship Propulsion

Numerical investigation of Lorentz force control on hypersonic inlet boundary layer separation

2011, 32 (1): 36-41   

Combustion , Heat and Mass Transfer

Coupling-looseness multidisciplinary design optimization of centrifugal compressor

2011, 32 (1): 42-46   

Analysis of the core driven fan stage with compact aerodynamic configuration

2011, 32 (1): 47-53   

Experiment on granularity peculiarity of condensed particlesin the chamber of SRM under aggregation condition

2011, 32 (1): 54-58   

Control methods of low frequency combustion instabilities in a dump combustor

2011, 32 (1): 59-64   

Discussion for evaluation of connected-pipe ramjet combustor performance parameters

2011, 32 (1): 65-69   

Experiments on vitiated air effects of ethylene-fueled supersonic combustion

2011, 32 (1): 70-75   

Investigation of triple impinging gas-gas injector mixing flowfield flow visualization

2011, 32 (1): 76-79   

Numerical and experimental study on multi-element gas-gas injector combustors

2011, 32 (1): 80-85   

Numerical analysis of vortex core flow in spinning solid rocket motor

2011, 32 (1): 86-90   

Design of scramjet nozzle based on streamline tracing technique

2011, 32 (1): 91-96   

Investigation on the effects of nozzles with different convergent-divergent angle on PDE performance

2011, 32 (1): 97-102   

Unsteady process of aerodynamic throat for solid rocket motor

2011, 32 (1): 103-108   

Material,Propellant and Fuel

Strength criterion based on accumulative damage for double-base propellant and experiment

2011, 32 (1): 109-112   

Flow structure measurement in a trapezoid duct with incline impingement jets near the leading edge

2011, 32 (1): 113-118   

Numerical simulation of regeneraive cooling flow and heat transfer with nonequilibrium flow

2011, 32 (1): 119-124   

Flow and heat transfer characteristics of “impingement-film cooling”configuration in limited space of rotating blade

2011, 32 (1): 125-129   

Methods for simultaneous measuring processes of combustion oscillations

2011, 32 (1): 130-134   

Real-time vibration monitoring algorithm and system design for high-speed turbopump

2011, 32 (1): 135-139   

Gas-path component fault diagnosis based on grayrelational analysis for aero-engine

2011, 32 (1): 140-145   

New Propulsion System

Experiment on flow field and thrust induced by plasma actuators

2011, 32 (1): 146-150