TY - JOUR
T1 - Verification of the numerical analysis using a collocated grid system directly solving the quasi-inviscid incompressible flow around a symmetric airfoil
AU - Suzuki, Hiroki
AU - Watanabe, Masaya
AU - Hasegawa, Yutaka
AU - Mochizuki, Shinsuke
N1 - Funding Information:
The authors acknowledge Professor Y. Morinishi (Nagoya Institute of Technology) and Associate Professor T. Ushijima (Nagoya Institute of Technology) for their valuable comments on this study. The present study was supported in part by the Japanese Ministry of Education, Culture, Sports, Science and Technology through Grants-in-Aid (Nos. 18K03932 and 18H01369).
Publisher Copyright:
© 2020 Published under licence by IOP Publishing Ltd.
PY - 2020/9/28
Y1 - 2020/9/28
N2 - The present study describes the results of validating a high-quality computational scheme of kinetic energy conservation characteristics under a collocated grid system. In the present study, the pseudo-inviscid incompressible flow around the Kármán-Trefftz airfoil is analyzed. In this analysis, the kinetic energy conservation error is reduced by temporally evolving the governing equation using pressure increments in fractional steps. This sufficient conservation of kinetic energy is validated using an inviscid homogeneous isotropic fluctuation field. The velocity field obtained by this analysis is compared to that of the potential flow obtained using the Kármán-Trefftz airfoil. The numerical analysis is also validated using the lift coefficient profile as a function of a small angle of attack.
AB - The present study describes the results of validating a high-quality computational scheme of kinetic energy conservation characteristics under a collocated grid system. In the present study, the pseudo-inviscid incompressible flow around the Kármán-Trefftz airfoil is analyzed. In this analysis, the kinetic energy conservation error is reduced by temporally evolving the governing equation using pressure increments in fractional steps. This sufficient conservation of kinetic energy is validated using an inviscid homogeneous isotropic fluctuation field. The velocity field obtained by this analysis is compared to that of the potential flow obtained using the Kármán-Trefftz airfoil. The numerical analysis is also validated using the lift coefficient profile as a function of a small angle of attack.
UR - http://www.scopus.com/inward/record.url?scp=85093697546&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85093697546&partnerID=8YFLogxK
U2 - 10.1088/1742-6596/1633/1/012028
DO - 10.1088/1742-6596/1633/1/012028
M3 - Conference article
AN - SCOPUS:85093697546
VL - 1633
JO - Journal of Physics: Conference Series
JF - Journal of Physics: Conference Series
SN - 1742-6588
IS - 1
M1 - 012028
T2 - 3rd International Conference on Mechanical, Electric and Industrial Engineering, MEIE 2020
Y2 - 18 June 2020
ER -