TY - GEN
T1 - Verification of the unified coordinate system by the method of manufactured solutions
AU - Nathan Woods, C.
AU - Starkey, Ryan P.
N1 - Publisher Copyright:
© 2015 American Institute of Aeronautics and Astronautics Inc. All rights reserved.
PY - 2014
Y1 - 2014
N2 - Although computational fluid dynamics has revolutionized aerodynamic analysis, it has remained less useful for preliminary design because of the dificulties associated with generating a computational grid. Hui's unified coordinate system has the potential to alleviate this concern by virtue of its automatically generated grid, but the method needs more study and development. We present a formal verification of the unified coordinate system in one dimension using both exact and manufactured solutions, including an integrative extension of the method of manufactured solutions which allows for discontinuities. This will provide the framework necessary to evaluate algorithmic improvements to the method, and provide confidence in the unified coordinate system as a tool for aerodynamic design, where its unique characteristics make it an extremely valuable alternative to traditional methods. First-order convergence is observed with a first-order method, while convergence is less for discontinuous solutions, as expected. The integrative method of manufactured solutions performs well, providing formal verification with a discontinuous, manufactured, solution.
AB - Although computational fluid dynamics has revolutionized aerodynamic analysis, it has remained less useful for preliminary design because of the dificulties associated with generating a computational grid. Hui's unified coordinate system has the potential to alleviate this concern by virtue of its automatically generated grid, but the method needs more study and development. We present a formal verification of the unified coordinate system in one dimension using both exact and manufactured solutions, including an integrative extension of the method of manufactured solutions which allows for discontinuities. This will provide the framework necessary to evaluate algorithmic improvements to the method, and provide confidence in the unified coordinate system as a tool for aerodynamic design, where its unique characteristics make it an extremely valuable alternative to traditional methods. First-order convergence is observed with a first-order method, while convergence is less for discontinuous solutions, as expected. The integrative method of manufactured solutions performs well, providing formal verification with a discontinuous, manufactured, solution.
UR - https://www.scopus.com/pages/publications/84938257341
M3 - Conference contribution
AN - SCOPUS:84938257341
T3 - 52nd Aerospace Sciences Meeting
BT - 52nd Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - 52nd Aerospace Sciences Meeting 2014
Y2 - 13 January 2014 through 17 January 2014
ER -