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A Study on Straight Flow Annular Combustor for Small Scale Turbojet Engine
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Changduk Kong,
Published/Copyright:
September 1, 2001
Published Online: 2001-09
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- Unsteady Analysis of a Time-Dependent Hot Streak in a Turbine Stage
- A Study on Straight Flow Annular Combustor for Small Scale Turbojet Engine
- Radial Cascade Unsteady Airfoil Theory
- Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation
- Multi-Objective Optimization of Turbomachinery Cascades for Minimum Loss, Maximum Loading, and Maximum Gap-to-Chord Ratio
- Some Unconventional Applications of Thermometers in Turbomachinery
- A Repeating Stage Model in Flow Predictions of Axial Flow Compressor Rear Stages
Articles in the same Issue
- CONTENTS
- Unsteady Analysis of a Time-Dependent Hot Streak in a Turbine Stage
- A Study on Straight Flow Annular Combustor for Small Scale Turbojet Engine
- Radial Cascade Unsteady Airfoil Theory
- Compressible Flow with Area Change and Friction as a Tool for Inlet Performance Evaluation
- Multi-Objective Optimization of Turbomachinery Cascades for Minimum Loss, Maximum Loading, and Maximum Gap-to-Chord Ratio
- Some Unconventional Applications of Thermometers in Turbomachinery
- A Repeating Stage Model in Flow Predictions of Axial Flow Compressor Rear Stages
