dc.creator | Petri, Larissa Alves | |
dc.creator | Sartori, Patrícia | |
dc.creator | Rogenski, Josuel Kruppa | |
dc.creator | Souza, Leandro Franco de | |
dc.date.accessioned | 2017-05-05T14:20:06Z | |
dc.date.accessioned | 2018-07-04T17:10:00Z | |
dc.date.available | 2017-05-05T14:20:06Z | |
dc.date.available | 2018-07-04T17:10:00Z | |
dc.date.created | 2017-05-05T14:20:06Z | |
dc.date.issued | 2015 | |
dc.identifier | Computer Methods in Applied Mechanics and Engineering,Amsterdam : Elsevier,v. 291, p. 266-279, 2015 | |
dc.identifier | 0045-7825 | |
dc.identifier | http://www.producao.usp.br/handle/BDPI/51272 | |
dc.identifier | 10.1016/j.cma.2015.04.001 | |
dc.identifier | http://dx.doi.org/10.1016/j.cma.2015.04.001 | |
dc.identifier.uri | http://repositorioslatinoamericanos.uchile.cl/handle/2250/1645549 | |
dc.description.abstract | The verification of a Direct Numerical Simulation code is carried out using the Method of Manufactured Solutions. Numerical
results from the code are also compared with experimental and Linear Stability Theory results in a boundary layer over an airfoil.
Displacement thickness, momentum thickness and shape factor are used to measure the boundary layer. Comparisons considering
the amplitude of the velocity disturbance caused by two-dimensional Tollmien–Schlichting waves are also made. The results show
the verification and validation of the Direct Numerical Simulation code. | |
dc.language | eng | |
dc.publisher | Elsevier | |
dc.publisher | Amsterdam | |
dc.relation | Computer Methods in Applied Mechanics and Engineering | |
dc.rights | Elsevier B.V | |
dc.rights | restrictedAccess | |
dc.subject | Boundary layer flow | |
dc.subject | High-order compact finite-difference scheme | |
dc.subject | Direct Numerical Simulation | |
dc.subject | Verification and validation | |
dc.subject | Method of Manufactured Solutions | |
dc.title | Verification and validation of a Direct Numerical Simulation code | |
dc.type | Artículos de revistas | |