TY - GEN
T1 - Direct numerical simulation of transcritical turbulent boundary layers at supercritical pressures with strong real fluid effects
AU - Kawai, Soshi
N1 - Funding Information:
This work was supported by Japan Society for the Promotion of Science (JSPS) Grant-in-Aid for Young Scientists (A) KAKENHI 26709066. Computer resources of the K computer was provided by the RIKEN Advanced Institute for Computational Science through the HPCI System Research project (Project ID: hp150035). The author gratefully acknowledge Mr. Hideyo Negishi for the technical assistance of tabulated NIST look-up table. The author are also grateful to Dr. Hiroshi Terashima and Dr. Hiroyuki Abe for valuable discussions.
Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All Rights Reserved.
PY - 2016
Y1 - 2016
N2 - Direct numerical simulation (DNS) of zero-pressure-gradient heated transcritical turbulent boundary layers on a flat plate at supercritical pressure conditions is conducted by solving the full compressible Navier-Stokes equations. To the best of my knowledge, the present DNS is the first DNS of zero-pressure-gradient flat-plate transcritical turbulent boundary layer. The peculiar interactions between the strongly non-linear real fluid effect at the transcritical condition and wall turbulence, and their resultant turbulence statistics and turbulent kinetic energy budget are investigated. The significant density fluctuations (formula presented) that originate from the strongly non-linear real fluid effects at the transcritical condition play an important role in determining the behaviors of transcritical turbulent boundary layers. Although there are considerable density fluctuation effects on the turbulence statistics, the mean density weighted Van Driest transformation of the mean velocity successfully collapses the mean velocity profiles to the same log-law as seen in ideal gas turbulent boundary layers. We also showed the validity of the semi-local wall coordinate y∗ = y/δ∗v and (formula presented) normalization for TKE budget terms in the transcritical turbulent boundary layers.
AB - Direct numerical simulation (DNS) of zero-pressure-gradient heated transcritical turbulent boundary layers on a flat plate at supercritical pressure conditions is conducted by solving the full compressible Navier-Stokes equations. To the best of my knowledge, the present DNS is the first DNS of zero-pressure-gradient flat-plate transcritical turbulent boundary layer. The peculiar interactions between the strongly non-linear real fluid effect at the transcritical condition and wall turbulence, and their resultant turbulence statistics and turbulent kinetic energy budget are investigated. The significant density fluctuations (formula presented) that originate from the strongly non-linear real fluid effects at the transcritical condition play an important role in determining the behaviors of transcritical turbulent boundary layers. Although there are considerable density fluctuation effects on the turbulence statistics, the mean density weighted Van Driest transformation of the mean velocity successfully collapses the mean velocity profiles to the same log-law as seen in ideal gas turbulent boundary layers. We also showed the validity of the semi-local wall coordinate y∗ = y/δ∗v and (formula presented) normalization for TKE budget terms in the transcritical turbulent boundary layers.
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U2 - 10.2514/6.2016-1934
DO - 10.2514/6.2016-1934
M3 - Conference contribution
AN - SCOPUS:85007485685
SN - 9781624103933
T3 - 54th AIAA Aerospace Sciences Meeting
BT - 54th AIAA Aerospace Sciences Meeting
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 54th AIAA Aerospace Sciences Meeting, 2016
Y2 - 4 January 2016 through 8 January 2016
ER -