TY - GEN
T1 - Numerical analysis of the jaxa standard model in high lift configuration
AU - Hendrickson, Karsten
AU - Agarwal, Ramesh K.
N1 - Publisher Copyright:
© 2021, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2021
Y1 - 2021
N2 - The flow phenomenon that occur in transport aircraft in take-off/landing (high-lift) configuration have proven to be challenging to model using Reynolds-averaged Navier-Stokes (RANS) equations with turbulence models. The complex interactions that occur between the fuselage, different elements of the wing, and the support hardware can result in numerical methods incorrectly approximating the body forces acting on the aircraft. In order to advance the prediction of high-lift flows, the AIAA established the High-Lift Prediction Workshops (HLPW), through which researchers from around the world could participate to share their results and learn about best CFD practices for accurate simulations. This research builds on the work from the 3rd HLPW by analyzing the effects of mesh, numerical method and turbulence models on the prediction of forces acting on the JAXA high lift model as well as the flow characteristics that result from the interaction of the different wing elements and support hardware.
AB - The flow phenomenon that occur in transport aircraft in take-off/landing (high-lift) configuration have proven to be challenging to model using Reynolds-averaged Navier-Stokes (RANS) equations with turbulence models. The complex interactions that occur between the fuselage, different elements of the wing, and the support hardware can result in numerical methods incorrectly approximating the body forces acting on the aircraft. In order to advance the prediction of high-lift flows, the AIAA established the High-Lift Prediction Workshops (HLPW), through which researchers from around the world could participate to share their results and learn about best CFD practices for accurate simulations. This research builds on the work from the 3rd HLPW by analyzing the effects of mesh, numerical method and turbulence models on the prediction of forces acting on the JAXA high lift model as well as the flow characteristics that result from the interaction of the different wing elements and support hardware.
UR - http://www.scopus.com/inward/record.url?scp=85100310145&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:85100310145
SN - 9781624106095
T3 - AIAA Scitech 2021 Forum
SP - 1
EP - 14
BT - AIAA Scitech 2021 Forum
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021
Y2 - 11 January 2021 through 15 January 2021
ER -