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Published/Copyright: May 9, 2022
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International Journal of Turbo & Jet-Engines
From the journal International Journal of Turbo & Jet-Engines Volume 39 Issue 2

Published Online: 2022-05-09
Published in Print: 2022-05-25

© 2022 Walter de Gruyter GmbH, Berlin/Boston

Articles in the same Issue

  1. Frontmatter
  2. Original Research Articles
  3. Investigations of Trenched Film Hole Orientation Angle on Film Cooling Effectiveness
  4. Jet Flow Control Using Semi-Circular Corrugated Tab
  5. Simulation of Use-Related Multi-Parameter Load Spectrum Based on Principal Component Analysis
  6. Characterization of Tandem Airfoil Configurations of Axial Compressors
  7. Research on Suppressing Vibration of Mistuning Cyclic-Periodic Structure
  8. Research on Power Regulation Schedule Control System for Turboprop Engine
  9. Enhancement of Full Coverage Film Cooling Effectiveness with Mixed Injection Holes
  10. CFD Analysis and Experimental Validation of the Flow Field in a Rib Roughed Turbine Internal Cooling Channel
  11. Perforated Wall in Controlling the Separation Bubble Due to Shock Wave –Boundary Layer Interaction
  12. Calculating Endogenous and Exogenous Exergy Destruction for an Experimental Turbojet Engine
  13. One-equation turbulence models applied to practical scramjet inlet
https://doi.org/10.1515/tjj-2022-frontmatter2

Articles in the same Issue

  1. Frontmatter
  2. Original Research Articles
  3. Investigations of Trenched Film Hole Orientation Angle on Film Cooling Effectiveness
  4. Jet Flow Control Using Semi-Circular Corrugated Tab
  5. Simulation of Use-Related Multi-Parameter Load Spectrum Based on Principal Component Analysis
  6. Characterization of Tandem Airfoil Configurations of Axial Compressors
  7. Research on Suppressing Vibration of Mistuning Cyclic-Periodic Structure
  8. Research on Power Regulation Schedule Control System for Turboprop Engine
  9. Enhancement of Full Coverage Film Cooling Effectiveness with Mixed Injection Holes
  10. CFD Analysis and Experimental Validation of the Flow Field in a Rib Roughed Turbine Internal Cooling Channel
  11. Perforated Wall in Controlling the Separation Bubble Due to Shock Wave –Boundary Layer Interaction
  12. Calculating Endogenous and Exogenous Exergy Destruction for an Experimental Turbojet Engine
  13. One-equation turbulence models applied to practical scramjet inlet
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