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Evaluation of an Euler Code with Non-Reflecting Boundary Conditions for the Analysis of 3D Flow in Compressors
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A. Fatsis,
Published/Copyright:
December 1, 1995
Published Online: 1995-12
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Editorial
- Thrust Vector Control Eyed for Passenger Aircraft: A Novel Methodology to Combine Jet-Engine Tests with Sub-Scale Proof-of-Concept Flight Tests
- Proposed Flight Testing Standards for Engine Thrust Vectoring to Maximize Kill Ratios, Post-Stall Agility and Flight Safety
- Dynamic Analysis and Experimental Correlation of a Gear Transmission System
- Evaluation of an Euler Code with Non-Reflecting Boundary Conditions for the Analysis of 3D Flow in Compressors
- Three-Dimensional LDA Measurements of the Flow Field Inside an Axial Gas Turbine Rotor
- Multivariable Control of the F-100 Turbofan Engine Using Edmunds' Method
Articles in the same Issue
- CONTENTS
- Editorial
- Thrust Vector Control Eyed for Passenger Aircraft: A Novel Methodology to Combine Jet-Engine Tests with Sub-Scale Proof-of-Concept Flight Tests
- Proposed Flight Testing Standards for Engine Thrust Vectoring to Maximize Kill Ratios, Post-Stall Agility and Flight Safety
- Dynamic Analysis and Experimental Correlation of a Gear Transmission System
- Evaluation of an Euler Code with Non-Reflecting Boundary Conditions for the Analysis of 3D Flow in Compressors
- Three-Dimensional LDA Measurements of the Flow Field Inside an Axial Gas Turbine Rotor
- Multivariable Control of the F-100 Turbofan Engine Using Edmunds' Method
