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Simple Formulae for Optimal Solidity of Two-Dimensional Compressor Cascades Based on Diffusion Concept
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C.-L. Liu,
Published/Copyright:
June 1, 1993
Published Online: 1993-06
©2011 by Walter de Gruyter GmbH & Co.
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Articles in the same Issue
- CONTENTS
- The Parametric Study of Ignition Process of a Fuel Droplet
- Analysis and Experimental Study on the Discharge Coefficient of Liner Holes
- Measurement Effects on the Calculation of In-FIight Thrust for an F404Turbofan Engine
- Simple Formulae for Optimal Solidity of Two-Dimensional Compressor Cascades Based on Diffusion Concept
- Viscous Gust Cascade Aerodynamics by a Locally Analytical Model
- Simulations of Free Shear Layers Using a Compressible k-є Model
Articles in the same Issue
- CONTENTS
- The Parametric Study of Ignition Process of a Fuel Droplet
- Analysis and Experimental Study on the Discharge Coefficient of Liner Holes
- Measurement Effects on the Calculation of In-FIight Thrust for an F404Turbofan Engine
- Simple Formulae for Optimal Solidity of Two-Dimensional Compressor Cascades Based on Diffusion Concept
- Viscous Gust Cascade Aerodynamics by a Locally Analytical Model
- Simulations of Free Shear Layers Using a Compressible k-є Model
