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Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
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Zhao-chun Wu,
Published/Copyright:
March 1, 2006
Published Online: 2006-03
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
- A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
- Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
- Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
- Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
- Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor
Articles in the same Issue
- CONTENTS
- Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
- A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
- Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
- Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
- Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
- Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor
