The influences of wind angles on the behavior of a high-speed train were investigated using a scaled-down wind tunnel model (1:8 scale) at the wind angles of 0°, 5.14°, 10.2°, 15.11°, and 19.8°. Based on the experimental results elicited at different Reynolds numbers (9.44 × 105, 1.26 × 106, 1.57 × 106, and 1.89 × 106, corresponding to the wind speeds of 30 m/s, 40 m/s, 50 m/s, and 60 m/s, respectively), the speed of 60 m/s was determined as optimal for wind tunnel tests. The effects of the incoming flow angles on the pressure distribution of the train's streamlined zone and the aerodynamic forces of the train were analyzed. Results show that the pressure coefficients on the leeward side and the symmetrical plane profile curve of the streamlined zone decreased as the wind angle increased. However, the change in the windward side was opposite to that of the leeward side. The lateral and the absolute value of the lift forces increased rapidly as a function of the wind angle, while the drag force was maximized when the wind angle was 15.11°, followed by subsequent decreases at increasing wind angles. •Influence of the wind angle on the aerodynamic performance of a high-speed train was investigated.•Influence of Reynolds number on the aerodynamic performance of high-speed train was investigated.•The boundary layer thickness along the train and ballast was measured and presented.•Pressure distributions along longitude direction and different cross-sections on train's streamlined zone were analyzed.