Improvement to numerical predictions of aerodynamic flows using experimental data assimilation

G. Barakos, D. Drikakis, W. Lefebre

Research output: Contribution to journalArticlepeer-review

Abstract

The idea of experimental data assimilation is investigated in the context of aerodynamic computations of turbulent compressible flows over airfoils. Two cases are considered: the subsonic flow around the ONERA-A airfoil; and the transonic flow around the RAE-2822 airfoil. The wall pressure-coefficient distribution, and the velocity and turbulent kinetic energy profiles are observed at various positions over the airfoil.

Original languageEnglish
Pages (from-to)611-614
Number of pages4
JournalJournal of Aircraft
Volume36
Issue number3
DOIs
Publication statusPublished - 1 Jan 1999
Externally publishedYes

Fingerprint

Dive into the research topics of 'Improvement to numerical predictions of aerodynamic flows using experimental data assimilation'. Together they form a unique fingerprint.

Cite this