Integral Theory for Turbulent Base Flows at Subsonic and Supersonic Speeds

Integral Theory for Turbulent Base Flows at Subsonic and Supersonic Speeds

<p>The integral near wake analysis of Reeves and Lees developed for supersonic laminar base flows is extended to the case of fully turbulent separated adiabatic flow behind a rearward facing step at both subsonic and supersonic speeds. A turbulent eddy viscosity model is formulated for the she...

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Bibliographic Details
Main Author: Alber, Irwin Emanuel
Format: Others
Published: 1967
Online Access:https://thesis.library.caltech.edu/4317/3/alber_ie_1967.pdf
Alber, Irwin Emanuel (1967) Integral Theory for Turbulent Base Flows at Subsonic and Supersonic Speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/0YEZ-H062. https://resolver.caltech.edu/CaltechETD:etd-10302003-141417 <https://resolver.caltech.edu/CaltechETD:etd-10302003-141417>

Internet

https://thesis.library.caltech.edu/4317/3/alber_ie_1967.pdf
Alber, Irwin Emanuel (1967) Integral Theory for Turbulent Base Flows at Subsonic and Supersonic Speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/0YEZ-H062. https://resolver.caltech.edu/CaltechETD:etd-10302003-141417 <https://resolver.caltech.edu/CaltechETD:etd-10302003-141417>

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