Throughflow in axial turbomachines with variable wall geometry

Throughflow in axial turbomachines with variable wall geometry

The theory of three-dimensional flow in axial turbomachines was extended to include the effects of variable hub and tip radii such as occur in the entrance stages of conventional axial flow compressors and, to a larger extent, in mixed flow compressors. The problem is simplified by assuming an infin...

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Bibliographic Details
Main Author: Oates, Gordon C.
Format: Others
Published: 1959
Online Access:https://thesis.library.caltech.edu/657/1/Oates_gc_1959.pdf
Oates, Gordon C. (1959) Throughflow in axial turbomachines with variable wall geometry. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/ZR3D-NR88. https://resolver.caltech.edu/CaltechETD:etd-02172006-093110 <https://resolver.caltech.edu/CaltechETD:etd-02172006-093110>

Internet

https://thesis.library.caltech.edu/657/1/Oates_gc_1959.pdf
Oates, Gordon C. (1959) Throughflow in axial turbomachines with variable wall geometry. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/ZR3D-NR88. https://resolver.caltech.edu/CaltechETD:etd-02172006-093110 <https://resolver.caltech.edu/CaltechETD:etd-02172006-093110>

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