Supersonic flow through cascades, with application to diffusers

Supersonic flow through cascades, with application to diffusers

Supersonic flow through a two-dimensional cascade of airfoils is discussed from the point of view of one-dimensional gas dynamics. Two generalizations to compressible flow of the usual velocity vector diagrams are discussed, namely the Mach vector and the reduced velocity vector diagram. A relative...

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Bibliographic Details
Main Author: Buhler, Rolf Dietrich
Format: Others
Published: 1948
Online Access:https://thesis.library.caltech.edu/4934/1/Buhler_rd_1948.pdf
Buhler, Rolf Dietrich (1948) Supersonic flow through cascades, with application to diffusers. Engineer's thesis, California Institute of Technology. doi:10.7907/FJEG-RM29. https://resolver.caltech.edu/CaltechETD:etd-12102008-131330 <https://resolver.caltech.edu/CaltechETD:etd-12102008-131330>

Internet

https://thesis.library.caltech.edu/4934/1/Buhler_rd_1948.pdf
Buhler, Rolf Dietrich (1948) Supersonic flow through cascades, with application to diffusers. Engineer's thesis, California Institute of Technology. doi:10.7907/FJEG-RM29. https://resolver.caltech.edu/CaltechETD:etd-12102008-131330 <https://resolver.caltech.edu/CaltechETD:etd-12102008-131330>

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