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Performance Prediction of Subsonic Vaned Diffusers Using an Integral Boundary Layer Method
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Ernesto Benini,
Published/Copyright:
June 1, 2007
Published Online: 2007-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Experimental Studies on Hydrodynamics of Recirculating Fluidized Beds
- Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel
- Numerical Simulation of Plane Mixing Layer by Three-Dimensional Vortex Method
- Performance Prediction of Subsonic Vaned Diffusers Using an Integral Boundary Layer Method
- Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours
- A Contribution to the Analysis of the Performance of the Gas Turbine Using Simulation
- Numerical Studies of a Novel Vortex Combustor
Articles in the same Issue
- CONTENTS
- Experimental Studies on Hydrodynamics of Recirculating Fluidized Beds
- Dust-Induced Deterioration of Compressor First Stage Blades in Supersonic Cascade Erosion Wind Tunnel
- Numerical Simulation of Plane Mixing Layer by Three-Dimensional Vortex Method
- Performance Prediction of Subsonic Vaned Diffusers Using an Integral Boundary Layer Method
- Technical Paper: Design Methods for Axisymmetric Supersonic Nozzle Contours
- A Contribution to the Analysis of the Performance of the Gas Turbine Using Simulation
- Numerical Studies of a Novel Vortex Combustor
