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Volume 43,Issue 5,2017 Table of Contents
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Contents
Analysis of Structural and Dynamical Characteristic Parameters of External Pipes for Aeroengine
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A Promoted Design Approach for Unknown Input Observer
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Numerical Study on Influence of Width of Guide Vane on Performance of Pre-Swirl System
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Application of 32 bit Fixed-point Arithmetic Library IQmath in FADEC System of Aeroengine
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Design of Acceleration Controller to a Turbofan Engine Using N-dot Method
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Robustness Optimization Design of Radial Deformation for Turbine Rotor
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Research and Application on Reliability Calculation Model of a Gear Based on Strength Reduction
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Improvement of Constitutive Model for GH901 Material Based on Chaboche Theory
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Research on Overall Design Scheme of Control System of Test Bed Experimental for a Intercooled Gas Turbine
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Fault Diagnosis of Gas Path Sonsor for Turbofan Engine
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Research on Aeroengine Fuel Nozzle Spray Angle Masurement
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Application of Gas Analysis Method on High Temperature Rise Full Annular Combustor Outlet Temperature Field Test
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Analysis on Dimension Tolerance Design of Non-circular Hole of Labyrinth Disk for an Aeroengine
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Design Requirements Analysis and Indicators Determination Strategy of Aeroengine Cryogenic Shell
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Research on Matching Method of Engine Model based on Test Data
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