An approximate method of calculating three-dimensional, compressible flow in axial turbomachines

An approximate method of calculating three-dimensional, compressible flow in axial turbomachines

The two principal existing methods of calculating axially-symmetric compressible flow in turbomachines are: (1) a simplified one-dimensional analysis, and (2) numerical methods using the complete or linearized flow equations. The first is not satisfactory for multi-stage turbines with appreciable wa...

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Bibliographic Details
Main Author: Holmquist, Carl Oreal
Format: Others
Published: 1953
Online Access:https://thesis.library.caltech.edu/1468/1/Holmquist_co_1953.pdf
Holmquist, Carl Oreal (1953) An approximate method of calculating three-dimensional, compressible flow in axial turbomachines. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/3FB2-G132. https://resolver.caltech.edu/CaltechETD:etd-04232003-115022 <https://resolver.caltech.edu/CaltechETD:etd-04232003-115022>

Internet

https://thesis.library.caltech.edu/1468/1/Holmquist_co_1953.pdf
Holmquist, Carl Oreal (1953) An approximate method of calculating three-dimensional, compressible flow in axial turbomachines. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/3FB2-G132. https://resolver.caltech.edu/CaltechETD:etd-04232003-115022 <https://resolver.caltech.edu/CaltechETD:etd-04232003-115022>

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