TY - JOUR
T1 - Discrete integration for measuring aerodynamic loads on trains in crosswinds − realizable strategies of discretization and discrete integration
AU - Gao, Hongrui
AU - Liu, Tanghong
AU - Liu, Zhiqi
AU - Huo, Xiaoshuai
AU - Zhang, Jie
AU - Wang, Xinran
AU - Chen, Zhengwei
N1 - Funding Information:
This work was supported by the Natural Science Foundation of Hunan Province, China (Grant numbers 2022JJ30727 and 2020JJ4737 ), the Science and Technology Innovation Program of Hunan Province, China (Grant No. 2022RC3040 ), the Technology Research and Development Program of China Railway Urumqi Group Co., Ltd. (Grant No. 2022-kj-70 ), China Scholarship Council (Grant No. 202206370140 ), and the Fundamental Research Funds for the Central Universities of Central South University (Grant No. 2022ZZTS0630 ). This work was carried out in part using computing resources at the High Performance Computing Center of Central South University.
Funding Information:
This work was supported by the Natural Science Foundation of Hunan Province, China (Grant numbers 2022JJ30727 and 2020JJ4737), the Science and Technology Innovation Program of Hunan Province, China (Grant No. 2022RC3040), the Technology Research and Development Program of China Railway Urumqi Group Co. Ltd. (Grant No. 2022-kj-70), China Scholarship Council (Grant No. 202206370140), and the Fundamental Research Funds for the Central Universities of Central South University (Grant No. 2022ZZTS0630). This work was carried out in part using computing resources at the High Performance Computing Center of Central South University.
Publisher Copyright:
© 2023 Elsevier Ltd
PY - 2023/7
Y1 - 2023/7
N2 - Discrete integration occupies an important place in train aerodynamic tests in crosswinds. Improved delayed detached eddy simulations based on shear stress transport k-ω turbulence models were carried out to calculate the side force, lift, rolling moment around the lee rail, and surface pressure on bluff and streamlined vehicles. The changepoints and piecewise linearities of the pressure coefficients were evaluated, and the maximum coefficient of determination in the elements was 0.9973. A realizable strategy of the discretization based on the Lagrange rectangular elements was suggested, including the largest lengths and numbers of the elements. From this, a strategy of the discrete integration was presented to measure the aerodynamic loads, considering the real orientation of the elements. The maximum errors of the mean aerodynamic load coefficients of the bluff and streamlined vehicles were 4.1% and 2.2% (except the mean lift coefficient of the bluff vehicle), respectively. The errors were less than those in the previous studies, especially for the streamlined vehicle, which reduced by up to 8.7%. The unsteady aerodynamic loads with no delay obtained by the strategies were near to natural ones in the frequency range that people would be concerned about in crosswinds (at the Strouhal number of less than 0.4). Some suggestions were made for using the strategies in the full-scale tests and model tests, which provided a foundation for further studies of the running safety in natural crosswinds.
AB - Discrete integration occupies an important place in train aerodynamic tests in crosswinds. Improved delayed detached eddy simulations based on shear stress transport k-ω turbulence models were carried out to calculate the side force, lift, rolling moment around the lee rail, and surface pressure on bluff and streamlined vehicles. The changepoints and piecewise linearities of the pressure coefficients were evaluated, and the maximum coefficient of determination in the elements was 0.9973. A realizable strategy of the discretization based on the Lagrange rectangular elements was suggested, including the largest lengths and numbers of the elements. From this, a strategy of the discrete integration was presented to measure the aerodynamic loads, considering the real orientation of the elements. The maximum errors of the mean aerodynamic load coefficients of the bluff and streamlined vehicles were 4.1% and 2.2% (except the mean lift coefficient of the bluff vehicle), respectively. The errors were less than those in the previous studies, especially for the streamlined vehicle, which reduced by up to 8.7%. The unsteady aerodynamic loads with no delay obtained by the strategies were near to natural ones in the frequency range that people would be concerned about in crosswinds (at the Strouhal number of less than 0.4). Some suggestions were made for using the strategies in the full-scale tests and model tests, which provided a foundation for further studies of the running safety in natural crosswinds.
KW - Aerodynamic load coefficients
KW - Crosswinds
KW - Discrete integration
KW - Discretization
KW - Lagrange rectangular elements
KW - Surface pressure distributions
UR - http://www.scopus.com/inward/record.url?scp=85156210743&partnerID=8YFLogxK
U2 - 10.1016/j.measurement.2023.112967
DO - 10.1016/j.measurement.2023.112967
M3 - Journal article
AN - SCOPUS:85156210743
SN - 0263-2241
VL - 216
JO - Measurement: Journal of the International Measurement Confederation
JF - Measurement: Journal of the International Measurement Confederation
M1 - 112967
ER -