Two-point measurements in the wake of a compressor cascade
- 15 June 1998
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- A four-sensor hot-wire probe system for three-component velocity measurementExperiments in Fluids, 1998
- Turbulence structure of the flow downstream of a compressor cascade with tip leakagePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Turbulence structure resulting from a perpendicular airfoil-vortex interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- The structure and development of a wing-tip vortexJournal of Fluid Mechanics, 1996
- Phase-averaging in the turbulent far-wakeExperiments in Fluids, 1989