TY - JOUR
T1 - Quantifying the influence of vortex instability on mean velocity field statistics of wingtip vortex
AU - Cheng, Zepeng
AU - Pan, Chong
AU - Wang, Jiangsheng
N1 - Publisher Copyright:
© The Chinese Society of Theoretical and Applied Mechanics and Springer-Verlag GmbH Germany, part of Springer Nature 2024.
PY - 2024/11
Y1 - 2024/11
N2 - During its evolution to the far field, the wingtip vortex exhibits complex instability behaviors such as long-wave/short-wave instability and vortex wandering. However, the quantification influence of vortex instability on its velocity field statistics has not been well investigated. To this end, experimental measurements of a canonical wingtip vortex generated by an elliptical wing under various angles of attack and Reynolds numbers were conducted using particle image velocimetry. It is found that the streamwise variation of wandering amplitude presents an exponential growth within the middle-to-far wake region and asymptotically saturates to 10−1b in the far wake, which differs from the previous report of a linear growth trend in the near-wake region. Further, two average methods, i.e., time average (TA) and ensemble average (EA), were adopted to compare the velocity field statistics. In both TA- and EA-obtained flow fields, the vortex radius rc, peak vorticity Ωxp, and vortex circulation Γ all demonstrate a power-law scaling with respect to the streamwise location, i.e., rc∝xkr,Ωxp∝x−kω, and Γ∝x−kΓ, respectively. For a full rolling-up wingtip vortex in the middle-to-far wake region, the fact that kΓ = kω − 2kr demonstrates that the vortex circulation can be scaled as Γ=Ωxp(rc)2. On the other hand, TA overestimates the decay rate of peak vorticity kω and the growth rate of vortex radius kr. Furthermore, the TA-introduced bias level of the peak vorticity and vortex radius is found to be scaled with an empirical scaling between the wandering amplitude by a power law, respectively. These findings provide significant practical value for detecting wake vortex in wake vortex spacing systems.
AB - During its evolution to the far field, the wingtip vortex exhibits complex instability behaviors such as long-wave/short-wave instability and vortex wandering. However, the quantification influence of vortex instability on its velocity field statistics has not been well investigated. To this end, experimental measurements of a canonical wingtip vortex generated by an elliptical wing under various angles of attack and Reynolds numbers were conducted using particle image velocimetry. It is found that the streamwise variation of wandering amplitude presents an exponential growth within the middle-to-far wake region and asymptotically saturates to 10−1b in the far wake, which differs from the previous report of a linear growth trend in the near-wake region. Further, two average methods, i.e., time average (TA) and ensemble average (EA), were adopted to compare the velocity field statistics. In both TA- and EA-obtained flow fields, the vortex radius rc, peak vorticity Ωxp, and vortex circulation Γ all demonstrate a power-law scaling with respect to the streamwise location, i.e., rc∝xkr,Ωxp∝x−kω, and Γ∝x−kΓ, respectively. For a full rolling-up wingtip vortex in the middle-to-far wake region, the fact that kΓ = kω − 2kr demonstrates that the vortex circulation can be scaled as Γ=Ωxp(rc)2. On the other hand, TA overestimates the decay rate of peak vorticity kω and the growth rate of vortex radius kr. Furthermore, the TA-introduced bias level of the peak vorticity and vortex radius is found to be scaled with an empirical scaling between the wandering amplitude by a power law, respectively. These findings provide significant practical value for detecting wake vortex in wake vortex spacing systems.
KW - PIV
KW - Vortex flow
KW - Vortex instability
KW - Wingtip vortex
UR - https://www.scopus.com/pages/publications/85208654303
U2 - 10.1007/s10409-024-24085-x
DO - 10.1007/s10409-024-24085-x
M3 - 文章
AN - SCOPUS:85208654303
SN - 0567-7718
VL - 40
JO - Acta Mechanica Sinica/Lixue Xuebao
JF - Acta Mechanica Sinica/Lixue Xuebao
IS - 11
M1 - 324085
ER -