A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery

D. Günes,; M. Mengütürk,

doi:10.1515/TJJ.1985.2.4.307

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A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery

D. Günes, and M. Mengütürk,

Published/Copyright: December 1, 1985

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From the journal International Journal of Turbo and Jet Engines Volume 2 Issue 4

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Günes,, D. and Mengütürk,, M.. "A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery" International Journal of Turbo and Jet Engines, vol. 2, no. 4, pp. 307-314. https://doi.org/10.1515/TJJ.1985.2.4.307

Günes,, D. & Mengütürk,, M. (). A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery. International Journal of Turbo and Jet Engines, 2(4), 307-314. https://doi.org/10.1515/TJJ.1985.2.4.307

Günes,, D. and Mengütürk,, M. () A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery. International Journal of Turbo and Jet Engines, Vol. 2 (Issue 4), pp. 307-314. https://doi.org/10.1515/TJJ.1985.2.4.307

Günes,, D. and Mengütürk,, M.. "A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery" International Journal of Turbo and Jet Engines 2, no. 4 (): 307-314. https://doi.org/10.1515/TJJ.1985.2.4.307

Günes, D, Mengütürk, M. A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery. International Journal of Turbo and Jet Engines. ;2(4): 307-314. https://doi.org/10.1515/TJJ.1985.2.4.307

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Published Online: 1985-12

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CONTENTS
Prediciton of Flow in Rotating Disc Systems Using the k-є Turbulence Model
Spray Characteristics of Two Combined Jet Atomizers
Nozzle Design and Integration in an Advanced Supersonic Fighter
Mass Flow Limitation of Supersonic Blade Rows Due to Leading Edge Blockage
Effect of Free Stream Turbulence on Flow Separation
Effect of Aspect Ratio on Energy Loss in Nozzle Blades of Small Power Turbines
A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery
The Role of the Heat-up Period in Fuel Drop Evaporation
Advanced Concepts in Small Helicopter Engine Air-Cooled Turbine Design
The Influence of Different Geometries for a Vaned Diffuser on the Pressure Distribution in a Centrifugal Compressor
Computer Calculation of Fan Erosion in Coal-fired Power Plants. Part 2: Axial Fans

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https://doi.org/10.1515/TJJ.1985.2.4.307

Articles in the same Issue

CONTENTS
Prediciton of Flow in Rotating Disc Systems Using the k-є Turbulence Model
Spray Characteristics of Two Combined Jet Atomizers
Nozzle Design and Integration in an Advanced Supersonic Fighter
Mass Flow Limitation of Supersonic Blade Rows Due to Leading Edge Blockage
Effect of Free Stream Turbulence on Flow Separation
Effect of Aspect Ratio on Energy Loss in Nozzle Blades of Small Power Turbines
A Finite Element Computer Code to Calculate Full 3-D Compressible Potential Flow in Turbomachinery
The Role of the Heat-up Period in Fuel Drop Evaporation
Advanced Concepts in Small Helicopter Engine Air-Cooled Turbine Design
The Influence of Different Geometries for a Vaned Diffuser on the Pressure Distribution in a Centrifugal Compressor
Computer Calculation of Fan Erosion in Coal-fired Power Plants. Part 2: Axial Fans