Article
Publicly Available
Frontmatter
Published/Copyright:
May 2, 2019
Published Online: 2019-05-02
Published in Print: 2019-05-01
© 2019 Walter de Gruyter GmbH, Berlin/Boston
Articles in the same Issue
- Frontmatter
- Editorial
- Jet-Engines Revised Dictionary for the 6th-Generation-R&D in a New Era
- Original Research Articles
- Off-Design Analysis of Transonic Bypass Fan Systems Using Streamline Curvature Through-Flow Method
- Predicting Lean Blowout and Emissions of Aircraft Engine Combustion Chamber Based on CRN
- Dielectric Barrier Discharge (DBD) Plasma Actuators for Flow Control in Turbine Engines: Simulation of Flight Conditions in the Laboratory by Density Matching
- Application of the Proper Orthogonal Decomposition Method in Analyzing Active Separation Control With Periodic Vibration Wall
- Model Predictive Control and Controller Parameter Optimisation of Combustion Instabilities
- Quasi-One-Dimensional Modeling and Analysis of RBCC Dual-Mode Scramjet Engine
- Investigation on the Performance of Forward Bending Fan
Articles in the same Issue
- Frontmatter
- Editorial
- Jet-Engines Revised Dictionary for the 6th-Generation-R&D in a New Era
- Original Research Articles
- Off-Design Analysis of Transonic Bypass Fan Systems Using Streamline Curvature Through-Flow Method
- Predicting Lean Blowout and Emissions of Aircraft Engine Combustion Chamber Based on CRN
- Dielectric Barrier Discharge (DBD) Plasma Actuators for Flow Control in Turbine Engines: Simulation of Flight Conditions in the Laboratory by Density Matching
- Application of the Proper Orthogonal Decomposition Method in Analyzing Active Separation Control With Periodic Vibration Wall
- Model Predictive Control and Controller Parameter Optimisation of Combustion Instabilities
- Quasi-One-Dimensional Modeling and Analysis of RBCC Dual-Mode Scramjet Engine
- Investigation on the Performance of Forward Bending Fan