Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor

Patrik P. Rautaheimo,; Esa J. Salminen,; Timo L. Siikonen,

doi:10.1515/TJJ.2003.20.2.155

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Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor

Patrik P. Rautaheimo, , Esa J. Salminen, and Timo L. Siikonen,

Published/Copyright: June 1, 2003

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From the journal International Journal of Turbo and Jet Engines Volume 20 Issue 2

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Vancouver

Rautaheimo,, Patrik P., Salminen,, Esa J. and Siikonen,, Timo L.. "Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor" International Journal of Turbo and Jet Engines, vol. 20, no. 2, pp. 155-170. https://doi.org/10.1515/TJJ.2003.20.2.155

Rautaheimo,, P., Salminen,, E. & Siikonen,, T. (). Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor. International Journal of Turbo and Jet Engines, 20(2), 155-170. https://doi.org/10.1515/TJJ.2003.20.2.155

Rautaheimo,, P., Salminen,, E. and Siikonen,, T. () Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor. International Journal of Turbo and Jet Engines, Vol. 20 (Issue 2), pp. 155-170. https://doi.org/10.1515/TJJ.2003.20.2.155

Rautaheimo,, Patrik P., Salminen,, Esa J. and Siikonen,, Timo L.. "Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor" International Journal of Turbo and Jet Engines 20, no. 2 (): 155-170. https://doi.org/10.1515/TJJ.2003.20.2.155

Rautaheimo, P, Salminen, E, Siikonen, T. Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor. International Journal of Turbo and Jet Engines. ;20(2): 155-170. https://doi.org/10.1515/TJJ.2003.20.2.155

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https://doi.org/10.1515/TJJ.2003.20.2.155

Articles in the same Issue

CONTENTS
Integrated Propulsion-based Flight Control System Design for a Civil Transport Aircraft
Gust Response Analysis of a Turbine Cascade
Three Dimensional Navier-Stokes Analysis of a Rigid Wing Configuration
Probabilistic Analysis of Gas Turbine Field Performance
Performance Characteristics of S-Shaped Diffusers with Elliptical Cross-Section
Numerical Simulation of the Flow in the NASA Low-Speed Centrifugal Compressor
Optimal Measurement Parameter Selection of Turboprop Engine Using GPA Approach
Steady-state Performance Simulation of PT6A-62 Turboprop Engine Using SIMULINK®