Numerical Analysis of the Effect of Different Nose Shapes on Train Aerodynamic Performance

This study investigates the aerodynamic performance of various trains with different nose shapes, using as the design variables two angles α,β for the head shape and the bluntness angle γ, without crosswind. The effects on aerodynamic performance, such as the train drag coefficient, pressure distribution along the train surface, flow structures around the train and the wake, and head pressure pulse, are analyzed. The results indicate that the increase in the train nose length for flat shapes decreases the CD values by 21.47% and 19.11%, decreasing the high-pressure region in the leading head. The duck nose configuration emerges as a compromise between drag reduction and nose length. Increasing the angle γ, a further drag reduction of 8.5% is featured. Drag formation along the train is also analyzed. The steeper the variation in the geometry, the higher the peak intensity and the slope of the curve. Regarding the flow features around the train, two main counter-rotating vortices are captured in the wake. Moreover, the higher the nose length and the higher the bluntness angle γ, the weaker and narrower the wake. Again, a longer nose shape yields a softer jump in terms of pressure difference, crucial for train homologation and safety.

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Publication Details

Journal
Fluids
Published
2024-09-27
DOI
https://doi.org/10.3390/fluids9100225
Citations
3
Primary Topic
Aerodynamics and Fluid Dynamics Research
Type
article
Field-Weighted Citation Impact
3.90
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article

Numerical Analysis of the Effect of Different Nose Shapes on Train Aerodynamic Performance

L. Vigevano, Paolo Schito, Stefano Negri, Kerian Chauvin et al.
3 citations
Fluids
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article

Numerical Analysis of the Effect of Different Nose Shapes on Train Aerodynamic Performance

L. Vigevano, Paolo Schito, Stefano Negri, Kerian Chauvin, Gianluca Colavito, Eric Landolfi
article en
3 citations

Abstract

This study investigates the aerodynamic performance of various trains with different nose shapes, using as the design variables two angles α,β for the head shape and the bluntness angle γ, without crosswind. The effects on aerodynamic performance, such as the train drag coefficient, pressure distribution along the train surface, flow structures around the train and the wake, and head pressure pulse, are analyzed. The results indicate that the increase in the train nose length for flat shapes decreases the CD values by 21.47% and 19.11%, decreasing the high-pressure region in the leading head. The duck nose configuration emerges as a compromise between drag reduction and nose length. Increasing the angle γ, a further drag reduction of 8.5% is featured. Drag formation along the train is also analyzed. The steeper the variation in the geometry, the higher the peak intensity and the slope of the curve. Regarding the flow features around the train, two main counter-rotating vortices are captured in the wake. Moreover, the higher the nose length and the higher the bluntness angle γ, the weaker and narrower the wake. Again, a longer nose shape yields a softer jump in terms of pressure difference, crucial for train homologation and safety.

FluidsVol. 9(10)
École Supérieure des Techniques Aéronautiques et de Construction Automobile (FR), Politecnico di Milano (IT)
Openalex Percentile: Top 6%
Aerodynamics and Fluid Dynamics Research
3.90
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