Analysis of the stability of a flat-plate high-speed boundary layer with discrete roughness

Analysis of the stability of a flat-plate high-speed boundary layer with discrete roughness

Boundary-layer transition from a laminar to a turbulent regime is a critical driver in the design of high-speed vehicles. The aerothermodynamic loads associated with transitional or fully turbulent hypersonic boundary layers are several times higher than those associated with laminar flow. The prese...

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Bibliographic Details
Main Author: Padilla Montero, Ivan
Other Authors: Coussement, Axel
Format: Doctoral Thesis
Language:en
Published: Universite Libre de Bruxelles 2021
Subjects:
Mécanique des fluides
Aérodynamique hypersonique
Analyse numérique
Thermophysique
Technologie aéronautique
boundary-layer transition
discrete roughness
hypersonic flow
linear stability theory
BiGlobal
computational fluid dynamics
Online Access:https://dipot.ulb.ac.be/dspace/bitstream/2013/324490/3/PhD_thesis_Ivan_Padilla_Montero-29MAY2021.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/324490/5/contratPM.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/324490/4/ToC-PhD_thesis_Ivan_Padilla_Montero.pdf
http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/324490

Internet

https://dipot.ulb.ac.be/dspace/bitstream/2013/324490/3/PhD_thesis_Ivan_Padilla_Montero-29MAY2021.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/324490/5/contratPM.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/324490/4/ToC-PhD_thesis_Ivan_Padilla_Montero.pdf
http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/324490

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