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Generalized Variational Principle for Compressible S2-Flow in Mixed-Flow Turbomachinery Using Semi-Inverse Method
Published/Copyright:
June 1, 1998
Published Online: 1998-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Can Thrust Vectoring Save a Doomed Transport Jet?
- Jet Deflection Angles in Military, Civil and RPV Thrust Vectoring Aircraft
- A Family of Variational Principles for Compressible Rotational Blade-to-Blade Flow Using Semi-Inverse Method
- Generalized Variational Principle for Compressible S2-Flow in Mixed-Flow Turbomachinery Using Semi-Inverse Method
- Inviscid-Viscous Iterative Solution for Flowfield in Transonic Compressor Rotor
- Turbine Performance Increases Through Airfoil Clocking
- Ignition Behaviors of Fuel Droplets in a Hot Convective Flowfield
- Effect of Dump Gap on Velocity Distribution and Flow Split in a Prototype Reverse-Flow Gas Turbine Combustor
Articles in the same Issue
- CONTENTS
- Can Thrust Vectoring Save a Doomed Transport Jet?
- Jet Deflection Angles in Military, Civil and RPV Thrust Vectoring Aircraft
- A Family of Variational Principles for Compressible Rotational Blade-to-Blade Flow Using Semi-Inverse Method
- Generalized Variational Principle for Compressible S2-Flow in Mixed-Flow Turbomachinery Using Semi-Inverse Method
- Inviscid-Viscous Iterative Solution for Flowfield in Transonic Compressor Rotor
- Turbine Performance Increases Through Airfoil Clocking
- Ignition Behaviors of Fuel Droplets in a Hot Convective Flowfield
- Effect of Dump Gap on Velocity Distribution and Flow Split in a Prototype Reverse-Flow Gas Turbine Combustor
