TY - GEN
T1 - Numerical accuracy in RANS computations of high-lift multi-element airfoil and aircraft configurations
AU - Antoniadis, Antonios F.
AU - Tsoutsanis, Panagiotis
AU - Drikakis, Dimitris
PY - 2015/1/1
Y1 - 2015/1/1
N2 - This paper presents the application of high-order finite volume methods in conjunction with unstructured grids for aeronautical flows. The numerical schemes comprise the Monotone-Upstream Central Scheme for Conservation Laws (MUSCL) and the Weighted Essentially Non-Oscillatory (WENO) scheme for mixed-element unstructured grids in two and three space dimensions. The aim of the present work is to assess the accuracy and efi- ciency of the above schemes in Reynolds-Averaged Navier-Stokes computations of external flows around a high-lift device and an aircraft configuration at landing conditions.
AB - This paper presents the application of high-order finite volume methods in conjunction with unstructured grids for aeronautical flows. The numerical schemes comprise the Monotone-Upstream Central Scheme for Conservation Laws (MUSCL) and the Weighted Essentially Non-Oscillatory (WENO) scheme for mixed-element unstructured grids in two and three space dimensions. The aim of the present work is to assess the accuracy and efi- ciency of the above schemes in Reynolds-Averaged Navier-Stokes computations of external flows around a high-lift device and an aircraft configuration at landing conditions.
UR - http://www.scopus.com/inward/record.url?scp=84980378812&partnerID=8YFLogxK
U2 - 10.2514/6.2015-0317
DO - 10.2514/6.2015-0317
M3 - Conference contribution
AN - SCOPUS:84980378812
SN - 9781624103438
T3 - 53rd AIAA Aerospace Sciences Meeting
BT - 53rd AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 53rd AIAA Aerospace Sciences Meeting, 2015
Y2 - 5 January 2015 through 9 January 2015
ER -