I. Supersonic Laminar Boundary Layer Along a Two-dimensional Adiabatic Curved Ramp. II. Non-Linear Stability Theory for a Laminar, Incompressible Wake

I. Supersonic Laminar Boundary Layer Along a Two-dimensional Adiabatic Curved Ramp. II. Non-Linear Stability Theory for a Laminar, Incompressible Wake

<p>In Part I, the integral method of Lees and Reeves is applied to study a supersonic laminar boundary layer along a two-dimensional adiabatic curved ramp. The present method of solution requires no prior knowledge of the separation point and can be used to treat relatively weak interaction, i...

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Bibliographic Details
Main Author: Ko, Denny Ru-sue
Format: Others
Language:en
Published: 1969
Online Access:https://thesis.library.caltech.edu/4484/1/Ko_dr_1969.pdf
Ko, Denny Ru-sue (1969) I. Supersonic Laminar Boundary Layer Along a Two-dimensional Adiabatic Curved Ramp. II. Non-Linear Stability Theory for a Laminar, Incompressible Wake. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/DM2V-N712. https://resolver.caltech.edu/CaltechETD:etd-11102003-093156 <https://resolver.caltech.edu/CaltechETD:etd-11102003-093156>

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https://thesis.library.caltech.edu/4484/1/Ko_dr_1969.pdf
Ko, Denny Ru-sue (1969) I. Supersonic Laminar Boundary Layer Along a Two-dimensional Adiabatic Curved Ramp. II. Non-Linear Stability Theory for a Laminar, Incompressible Wake. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/DM2V-N712. https://resolver.caltech.edu/CaltechETD:etd-11102003-093156 <https://resolver.caltech.edu/CaltechETD:etd-11102003-093156>

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