Show simple item record

dc.contributor.authorFernandez del Campo, Pablo
dc.contributor.authorNguyen, Ngoc Cuong
dc.contributor.authorPeraire, Jaime
dc.date.accessioned2018-04-27T21:40:23Z
dc.date.available2018-04-27T21:40:23Z
dc.date.issued2018-01
dc.identifier.isbn978-1-62410-524-1
dc.identifier.urihttp://hdl.handle.net/1721.1/115071
dc.description.abstractWe present a shock capturing method for unsteady laminar and turbulent flows. The proposed approach relies on physical principles to increase selected transport coefficients and resolve unstable sharp features, such as shock waves and strong thermal and shear gradients, over the smallest distance allowed by the discretization. In particular, we devise various sensors to detect when the shear viscosity, bulk viscosity and thermal conductivity of the fluid do not suffice to stabilize the numerical solution. In such cases, the transport coefficients are increased as necessary to optimally resolve these features with the available resolution. The performance of the method is illustrated through numerical simulation of external and internal flows in transonic, supersonic, and hypersonic regimes.en_US
dc.description.sponsorshipUnited States. Air Force. Office of Scientific Research (FA9550-16-1-0214)en_US
dc.description.sponsorshipPratt & Whitney Aircraft Companyen_US
dc.description.sponsorshipFundación Obra Social de La Caixaen_US
dc.description.sponsorshipMassachusetts Institute of Technology. Office of the Dean for Graduate Education (Zakhartchenko Fellowship)en_US
dc.language.isoen_US
dc.publisherAmerican Institute of Aeronautics and Astronautics (AIAA)en_US
dc.relation.isversionofhttps://arc.aiaa.org/doi/abs/10.2514/6.2018-0062en_US
dc.rightsCreative Commons Attribution-Noncommercial-Share Alikeen_US
dc.rights.urihttp://creativecommons.org/licenses/by-nc-sa/4.0/en_US
dc.sourcePablo Fernandezen_US
dc.titleA physics-based shock capturing method for unsteady laminar and turbulent flowsen_US
dc.typeArticleen_US
dc.identifier.citationFernandez, Pablo, Cuong Nguyen, and Jaime Peraire. “A Physics-Based Shock Capturing Method for Unsteady Laminar and Turbulent Flows.” 2018 AIAA Aerospace Sciences Meeting (January 7, 2018), Kissimmee, Florida, 2018.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronauticsen_US
dc.contributor.approverPablo Fernandezen_US
dc.contributor.mitauthorFernandez del Campo, Pablo
dc.contributor.mitauthorNguyen, Ngoc Cuong
dc.contributor.mitauthorPeraire, Jaime
dc.relation.journal2018 AIAA Aerospace Sciences Meetingen_US
dc.eprint.versionAuthor's final manuscripten_US
dc.type.urihttp://purl.org/eprint/type/ConferencePaperen_US
eprint.statushttp://purl.org/eprint/status/NonPeerRevieweden_US
dspace.orderedauthorsFernandez, Pablo; Nguyen, Cuong; Peraire, Jaimeen_US
dspace.embargo.termsNen_US
dc.identifier.orcidhttps://orcid.org/0000-0002-6291-4946
dc.identifier.orcidhttps://orcid.org/0000-0002-8556-685X
mit.licenseOPEN_ACCESS_POLICYen_US


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record