Hypersonic viscous-inviscid flow interactions including boundary layer separation on a flat plate at angle of attack

Hypersonic viscous-inviscid flow interactions including boundary layer separation on a flat plate at angle of attack

Experimental measurements of mean flow properties over the leeward surface and in the near wake of an adiabatic thin flat plate at an angle of attack of α = 15° were obtained at Mach 6 and Reynolds number based on the chord length of 186,000. The leading edge thickness is the predominant variable wh...

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Bibliographic Details
Main Author: Hulcher, Gregory D.
Format: Others
Published: 1972
Online Access:https://thesis.library.caltech.edu/6021/1/Hulcher_gd_1972.pdf
Hulcher, Gregory D. (1972) Hypersonic viscous-inviscid flow interactions including boundary layer separation on a flat plate at angle of attack. Engineer's thesis, California Institute of Technology. doi:10.7907/PZCP-FT88. https://resolver.caltech.edu/CaltechTHESIS:09032010-111033039 <https://resolver.caltech.edu/CaltechTHESIS:09032010-111033039>

Internet

https://thesis.library.caltech.edu/6021/1/Hulcher_gd_1972.pdf
Hulcher, Gregory D. (1972) Hypersonic viscous-inviscid flow interactions including boundary layer separation on a flat plate at angle of attack. Engineer's thesis, California Institute of Technology. doi:10.7907/PZCP-FT88. https://resolver.caltech.edu/CaltechTHESIS:09032010-111033039 <https://resolver.caltech.edu/CaltechTHESIS:09032010-111033039>

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