Experimental investigation of supersonic laminar, two-dimensional boundary layer separation in a compression corner with and without cooling

Experimental investigation of supersonic laminar, two-dimensional boundary layer separation in a compression corner with and without cooling

An experimental investigation of the boundary layer separation associated with a compression corner was conducted in the GALCIT Mach 6 wind tunnel, and a supplementary study was performed in the JPL supersonic wind tunnel. Special emphasis was placed on the development of a wind tunnel model which a...

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Bibliographic Details
Main Author: Lewis, John Eldon
Format: Others
Published: 1967
Online Access:https://thesis.library.caltech.edu/4587/1/Lewis_je_1967.pdf
Lewis, John Eldon (1967) Experimental investigation of supersonic laminar, two-dimensional boundary layer separation in a compression corner with and without cooling. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/R0FB-DD20. https://resolver.caltech.edu/CaltechETD:etd-11162005-102455 <https://resolver.caltech.edu/CaltechETD:etd-11162005-102455>

Internet

https://thesis.library.caltech.edu/4587/1/Lewis_je_1967.pdf
Lewis, John Eldon (1967) Experimental investigation of supersonic laminar, two-dimensional boundary layer separation in a compression corner with and without cooling. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/R0FB-DD20. https://resolver.caltech.edu/CaltechETD:etd-11162005-102455 <https://resolver.caltech.edu/CaltechETD:etd-11162005-102455>

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