The present database contains information on 11 different two-dimensional csacade geometries and the corresponding unsteady flow established by the vibrating blades. It is believed that this database is presently the most comprehensive database related to aeroelasticity in turbomachines in the open literature.

Contents

• Contents Update of STCF 4: Cambered turbine cascade in transonic flow


• STCF 11: Low pressure annular turbine cascade, subsonic and transonic off-design with separated flow


• STCF 1-10 according to
  

  Updated report on "Standard Configurations for Unsteady Flow Through Vibrating Axial-Flow Turbomachine-Cascades", Status as of July 1991, compiled by T. H. Fransson and J. M. Verdon: SC2110.92update.pdf (394 KB). Abstract Introduction and Objectives Standard Configurations First Standard Configuration: Compressor cascade in low subsonic flow Second Standard Configuration Third Standard Configuration Fourth Standard Configuration: Cambered turbine cascade in transonic flow Fifth Standard Configuration: Compressor cascade in high subsonic flow Sixth Standard Configuration Seventh Standard Configuration: Compressor cascade in supersonic flow Eighth Standard Configuration: Flat plate cascade in sub- and supersonic flow Ninth Standard Configuration: Double circular arc profiles in sub- and transonic flow Tenth Standard Configuration: Modified cambered NACA 0006 cascade in sub- and transonic flow Conclusions and Recommendations Acknowledgements

• Contact person
• Links to other databases in the field
• Publications:
  • Aerodynamics in turbomachines comparison of theoretical and experimental cascade results.pdf
  • Aerodynamics in turbomachines comparison of theoretical and experimental cascade results, APPENDIX A5.pdf