Article
Publicly Available
Frontmatter
Published/Copyright:
February 16, 2018
Published Online: 2018-2-16
Published in Print: 2018-2-15
© 2018 Walter de Gruyter GmbH, Berlin/Boston
Articles in the same Issue
- Frontmatter
- Mechanism of Film Cooling with One Inlet and Double Outlet Hole Injection at Various Turbulence Intensities
- State of Aircraft Turboshaft Engines by Means of Tribotechnical Diagnostic
- Theoretical Study of the Vibration Suppression on a Mistuned Bladed Disk Using a Bi-periodic Piezoelectric Network
- Effect of Axisymmetric Aft Wall Angle Cavity in Supersonic Flow Field
- A Generalized Method for the Comparable and Rigorous Calculation of the Polytropic Efficiencies of Turbocompressors
- Sliding Mode Fault Tolerant Control with Adaptive Diagnosis for Aircraft Engines
- Numerical Study on the Improvement of Oil Return Structure in Aero-Engine Bearing Chambers
- Numerical Investigation of Fuel Distribution Effect on Flow and Temperature Field in a Heavy Duty Gas Turbine Combustor
- A Novel Quasi-3D Method for Cascade Flow Considering Axial Velocity Density Ratio
Articles in the same Issue
- Frontmatter
- Mechanism of Film Cooling with One Inlet and Double Outlet Hole Injection at Various Turbulence Intensities
- State of Aircraft Turboshaft Engines by Means of Tribotechnical Diagnostic
- Theoretical Study of the Vibration Suppression on a Mistuned Bladed Disk Using a Bi-periodic Piezoelectric Network
- Effect of Axisymmetric Aft Wall Angle Cavity in Supersonic Flow Field
- A Generalized Method for the Comparable and Rigorous Calculation of the Polytropic Efficiencies of Turbocompressors
- Sliding Mode Fault Tolerant Control with Adaptive Diagnosis for Aircraft Engines
- Numerical Study on the Improvement of Oil Return Structure in Aero-Engine Bearing Chambers
- Numerical Investigation of Fuel Distribution Effect on Flow and Temperature Field in a Heavy Duty Gas Turbine Combustor
- A Novel Quasi-3D Method for Cascade Flow Considering Axial Velocity Density Ratio
