Article
Publicly Available
Frontmatter
Published/Copyright:
October 26, 2017
Published Online: 2017-10-26
Published in Print: 2017-10-25
© 2017 Walter de Gruyter GmbH, Berlin/Boston
Articles in the same Issue
- Frontmatter
- Expanded R&D by Jet-engine-steering Revolution
- Scientific Paper
- Switching LPV Control with Double-Layer LPV Model for Aero-Engines
- On-Board Real-Time Optimization Control for Turbo-Fan Engine Life Extending
- Investigation of Engine Oil-cooling Problem during Idle Conditions on Pusher Type Turbo Prop Aircraft
- Regulating Effect of Asymmetrical Impeller on the Flow Distributions of Double-sided Centrifugal Compressor
- Numerical Prediction of the Influence of Thrust Reverser on Aeroengine’s Aerodynamic Stability
- Performance Evaluation of an Experimental Turbojet Engine
- The Design and Semi-Physical Simulation Test of Fault-Tolerant Controller for Aero Engine
- The Ignition of Two Phase Detonation by a Branching Detonation Tube
- Tab Geometry Effect on Supersonic Elliptic Jet Control
Articles in the same Issue
- Frontmatter
- Expanded R&D by Jet-engine-steering Revolution
- Scientific Paper
- Switching LPV Control with Double-Layer LPV Model for Aero-Engines
- On-Board Real-Time Optimization Control for Turbo-Fan Engine Life Extending
- Investigation of Engine Oil-cooling Problem during Idle Conditions on Pusher Type Turbo Prop Aircraft
- Regulating Effect of Asymmetrical Impeller on the Flow Distributions of Double-sided Centrifugal Compressor
- Numerical Prediction of the Influence of Thrust Reverser on Aeroengine’s Aerodynamic Stability
- Performance Evaluation of an Experimental Turbojet Engine
- The Design and Semi-Physical Simulation Test of Fault-Tolerant Controller for Aero Engine
- The Ignition of Two Phase Detonation by a Branching Detonation Tube
- Tab Geometry Effect on Supersonic Elliptic Jet Control