TY - GEN
T1 - Advances in numerical methods for CREATE™-AV analysis tools
AU - Burgess, Nicholas K.
AU - Glasby, Ryan S.
PY - 2014
Y1 - 2014
N2 - This work considers advances in numerical methods for future air vehicle Computational Research and Engineering for Acquisition Tools and Environments (CREATE™-AV) computational fluid dynamics (CFD) solvers. CREATE™-AV is on the verge of adopting CFD methods that are beyond the current state of the art. In particular high-order spatial discretization methods for unstructured/semi-structured meshes are a large part of the future of CREATE™-AV computational fluid dynamics solvers. Adopting new spatial discretization methods is an involved process that motivates one to re-examine the CFD procedure as a whole. The goal of this work is to explain some emerging technologies that will enable enhanced accuracy, speed, robustness, and utility of CREATE™-AV software. The emerging technologies in this work include finite-element spatial integration techniques and full Newton solvers that are automatic and adapt to the flow solution state. Results of these techniques are shown for challenging two-dimensional test cases.
AB - This work considers advances in numerical methods for future air vehicle Computational Research and Engineering for Acquisition Tools and Environments (CREATE™-AV) computational fluid dynamics (CFD) solvers. CREATE™-AV is on the verge of adopting CFD methods that are beyond the current state of the art. In particular high-order spatial discretization methods for unstructured/semi-structured meshes are a large part of the future of CREATE™-AV computational fluid dynamics solvers. Adopting new spatial discretization methods is an involved process that motivates one to re-examine the CFD procedure as a whole. The goal of this work is to explain some emerging technologies that will enable enhanced accuracy, speed, robustness, and utility of CREATE™-AV software. The emerging technologies in this work include finite-element spatial integration techniques and full Newton solvers that are automatic and adapt to the flow solution state. Results of these techniques are shown for challenging two-dimensional test cases.
UR - http://www.scopus.com/inward/record.url?scp=84902827335&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84902827335
SN - 9781624102561
T3 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
BT - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 52nd AIAA Aerospace Sciences Meeting - AIAA Science and Technology Forum and Exposition, SciTech 2014
Y2 - 13 January 2014 through 17 January 2014
ER -