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Volume 51,Issue 1,2025 Table of Contents
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Contents
Development and Prospect of Aeroengine Testing Technology
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Review of Research on Energy Management Strategies for Hybrid Aircraft Propulsion System
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Review of Multi-Component Box Balance for Aeroengine Thrust Measurement
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Gas Turbine Intake System Resistance Characteristics Correction Method
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Stability Enhancement of Highly Loaded Fan with Position-Optimized Circumferential Casing Treatment Grooves
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Effects of Turbine Blade Airfoil Tolerances on Turbine Throat Area
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The Effect of Bend Section Radius on the Initiation Characteristics of a Reverse Flow Pulse Detonation Combustion Chamber
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Numerical Simulation of Internal Flow and Atomization Characteristics of Centrifugal Nozzle
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Radar Stealth Shaping Design for Cone of Integrated Afterburner with Axisymmetric Nozzle
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Influence of Radar Absorbing Coating Materials on Radar Scattering Characteristics of Engine Exhaust System
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Design Improvement of a Combustion Chamber Rigid Fuel Manifold Flow Characteristics
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Effect of Phase Combination of Residual Unbalance on Rotor Vibration Response of Turboprop Engines
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Active Identification Method of Counter-rotating Critical Speeds Based on “Gyroscopic Kinetic Energy”
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Machine-Learning-Based Fatigue Life Prediction Method for Welded Joints
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Simplified Cracked Body Modeling for Aeroengine Disk
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Influence of Rolling Bearing Radial Clearance on Dynamic Characteristics of Flexible Rotor System with Supporting Non-Concentricity
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Experimental Investigation on Small Crack Propagation Behaviors of Powder Metallurgy Superalloy FGH4099
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Influence of Labyrinth Seal on Transient Tip Clearance Simulation of Core Engine
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Improved YOLOv7 Damage Detection Method for Aeroengine Blade
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Main Bearing Condition Monitoring Method Based on Vibration and Oil Debris Information Fusion
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Low Pressure Turbine Rotor Blades Temperature Field Measurement at Simulated Altitude Conditions Using Long Working Distance Pyrometer
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A Nonlinear Modeling Method for a Rotor-Support System Based on Model Validation
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Rotor Vibration Monitoring Based on Adaptive Blade Tip Clearance Measurement
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Analysis of Cracking Mechanism of IC10 Alloy High Pressure Turbine Guide Vane
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Preparation and Reflectance Performance Simulation of New Carbon-Based Radar Absorbing Materials
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