Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor

William Oakes,; Pat Shook,; Ron McGuire,; Sanford Fleeter,

doi:10.1515/TJJ.1997.14.4.187

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Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor

William Oakes, , Pat Shook, , Ron McGuire, and Sanford Fleeter,

Published/Copyright: December 1, 1997

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From the journal International Journal of Turbo and Jet Engines Volume 14 Issue 4

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Harvard
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Oakes,, William, Shook,, Pat, McGuire,, Ron and Fleeter,, Sanford. "Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor" International Journal of Turbo and Jet Engines, vol. 14, no. 4, pp. 187-200. https://doi.org/10.1515/TJJ.1997.14.4.187

Oakes,, W., Shook,, P., McGuire,, R. & Fleeter,, S. (). Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor. International Journal of Turbo and Jet Engines, 14(4), 187-200. https://doi.org/10.1515/TJJ.1997.14.4.187

Oakes,, W., Shook,, P., McGuire,, R. and Fleeter,, S. () Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor. International Journal of Turbo and Jet Engines, Vol. 14 (Issue 4), pp. 187-200. https://doi.org/10.1515/TJJ.1997.14.4.187

Oakes,, William, Shook,, Pat, McGuire,, Ron and Fleeter,, Sanford. "Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor" International Journal of Turbo and Jet Engines 14, no. 4 (): 187-200. https://doi.org/10.1515/TJJ.1997.14.4.187

Oakes, W, Shook, P, McGuire, R, Fleeter, S. Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor. International Journal of Turbo and Jet Engines. ;14(4): 187-200. https://doi.org/10.1515/TJJ.1997.14.4.187

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Published Online: 1997-12

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Articles in the same Issue

CONTENTS
Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor
Special Features of the Combustion of a Propagating Flame in a Polydisperse Fuel Spray Cloud
Investigation of Hot Streak Temperature Ratio Scaling Effects
Shock Boundary Layer Interaction Structure
Investigation of Pressure Oscillations in Supersonic Cavity Flow
Editorial

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https://doi.org/10.1515/TJJ.1997.14.4.187

Articles in the same Issue

CONTENTS
Aerodynamic Performance and Instability Initiation of a High Speed Research Centrifugal Compressor
Special Features of the Combustion of a Propagating Flame in a Polydisperse Fuel Spray Cloud
Investigation of Hot Streak Temperature Ratio Scaling Effects
Shock Boundary Layer Interaction Structure
Investigation of Pressure Oscillations in Supersonic Cavity Flow
Editorial