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System

General Modeling Algorithm for Propeller MathematicalModel Based on Component Characteristics

2019, 40 (8): 1681-1692   DOI:10.13675/j.cnki. tjjs. 180511

Application of Exergy Analysis in SynergisticAir-Breathing Rocket Engine

2019, 40 (8): 1693-1701   DOI:10.13675/j.cnki. tjjs. 180542

Aero-thermodynamics

Investigation on Transient Response Characteristics ofFlow of Rotor-Stator Cavity

2019, 40 (8): 1702-1709   DOI:10.13675/j.cnki. tjjs. 180417

A Computational Method of Boundary Layer Blockage inAxial Compressors Based on CFD Results

2019, 40 (8): 1710-1719   DOI:10.13675/j.cnki. tjjs. 180492

Effects of Wall Temperature Ratio on ShockTrain in Cylindrical Isolator

2019, 40 (8): 1720-1726   DOI:10.13675/j.cnki. tjjs. 180493

Integrated Design of Intermediate Turbine DuctUsing Inverse Method

2019, 40 (8): 1727-1733   DOI:10.13675/j.cnki. tjjs. 180764

Research on Effects of Nonaxisymmetric Endwall Contouringon Blade Endwall Aerothermal Performance

2019, 40 (8): 1734-1742   DOI:10.13675/j.cnki. tjjs. 180513

Optimization Design of Composite Impeller of Aero-Centrifugal Pump Based on Particle Swarm Optimization

2019, 40 (8): 1743-1751   DOI:10.13675/j.cnki. tjjs. 180509

Experimental Research on Flow Characteristics of Bumpswith Different Compression Configurations

2019, 40 (8): 1752-1758   DOI:10.13675/j.cnki. tjjs. 180506

A Study of Flow Characteristics in Isolator with Effects ofBoundary Layer Suction and Oscillating Back Pressure

2019, 40 (8): 1759-1766   DOI:10.13675/j.cnki. tjjs. 180498

Application of CST Method on Modifying Leading Edgeof Axial-Flow Turbine Blade

2019, 40 (8): 1767-1779   DOI:10.13675/j.cnki. tjjs. 190063

Study of Improving Surge Margin for aSupersonic Compressor Stage

2019, 40 (8): 1780-1791   DOI:10.13675/j.cnki. tjjs. 180550

Entrainment Characteristics of Hollow Cone SprayDroplets in Crossflow

2019, 40 (8): 1792-1798   DOI:10.13675/j.cnki. tjjs. 180410

Experimental Investigation of Effects of Airflow Spliton the Characteristics of Dual-Axial Swirler

2019, 40 (8): 1799-1806   DOI:10.13675/j.cnki. tjjs. 180329

Numerical Study of Supersonic Combustion Flowwith Transverse Pulse Jet

2019, 40 (8): 1807-1816   DOI:10.13675/j.cnki. tjjs. 180406

Experimental Analysis on Characteristic and Boundary ofThermo-Acoustic Flow Instability in Hydrocarbon Fuel

2019, 40 (8): 1817-1823   DOI:10.13675/j.cnki. tjjs. 180474

Experimental Investigation on Spray Characteristic ofInternally-Staged Combustor

2019, 40 (8): 1824-1831   DOI:10.13675/j.cnki. tjjs. 180490

Prediction of Carbon Black Distribution in Multi-Stateof Small-Scale Reverse Flow Combustor

2019, 40 (8): 1832-1841   DOI:10.13675/j.cnki. tjjs. 180510

Experimental Study on Overall Cooling Effectiveness ofInclined Multihole under the Same Pressure Differential

2019, 40 (8): 1842-1849   DOI:10.13675/j.cnki. tjjs. 180531

Effects of Hydrogen Blending Ratio on CombustionCharacteristics of Micro-Lobed Burner

2019, 40 (8): 1850-1860   DOI:10.13675/j.cnki. tjjs. 180611

Structure, Strength and Reliablity

Method of Modal Separation and Damping ParameterIdentification of Each Mode of Multi-Modal VibrationAttenuation Signals in Time Domain

2019, 40 (8): 1861-1868   DOI:10.13675/j.cnki. tjjs. 180518

A Constitutive Model of Flexible Composites Used inBump of Particle Separator

2019, 40 (8): 1869-1875   DOI:10.13675/j.cnki. tjjs. 180520

Fatigue Analysis and Experimental Research for Thin-Walled Plates under Thermoacoustic Loading in Traveling Wave Tube

2019, 40 (8): 1876-1886   DOI:10.13675/j.cnki. tjjs. 180557

Test,Experiment and Control

Laser Diagnostic on Structure of Premixed SwirlingMulti-Nozzle Flame

2019, 40 (8): 1887-1894   DOI:10.13675/j.cnki. tjjs. 180543

Comparative Study on Modeling Methods of Special Control Valves in Altitude Simulation Test Facility

2019, 40 (8): 1895-1901   DOI:10.13675/j.cnki. tjjs. 180546

Flame Sensor Based on Resistance-TemperatureCharacteristic of Yttria-Stabilized Zirconia

2019, 40 (8): 1902-1911   DOI:10.13675/j.cnki. tjjs. 180586

Material,Propellant and Fuel

Impedance Characterization and Validation of Solid Propellant Based on Electro-Mechanical Impedance Method

2019, 40 (8): 1912-1920   DOI:10.13675/j.cnki. tjjs. 180521