2022
DOI: 10.1007/s00348-022-03546-y
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Wake-triggered secondary vortices over a cylinder/airfoil configuration

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Cited by 7 publications
(4 citation statements)
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“…Therefore, innovative design cannot be limited in terms of architecture. It must also contend with issues including the adaptability of the vehicle architecture, the effective coordination of numerous actuators, and safe operation in the event of a malfunction, all of which need to be considered while designing the chassis [7].…”
Section: Intelligent Automobile Wire Control Chassismentioning
confidence: 99%
See 1 more Smart Citation
“…Therefore, innovative design cannot be limited in terms of architecture. It must also contend with issues including the adaptability of the vehicle architecture, the effective coordination of numerous actuators, and safe operation in the event of a malfunction, all of which need to be considered while designing the chassis [7].…”
Section: Intelligent Automobile Wire Control Chassismentioning
confidence: 99%
“…Therefore, innovative design cannot be limited in terms of architecture. It must also contend with issues including the adaptability of the vehicle architecture, the effective coordination of numerous actuators, and safe operation in the event of a malfunction, all of which need to be considered while designing the chassis[7].In the context of the requirement of new energy vehicle lifetime, increasing premise and battery energy density temporarily no breakthrough progress, the other systems can streamline, reduce occupation volume, and reduce the weight of the parts is the trend.…”
mentioning
confidence: 99%
“…Various methods, both passive and active, have been proposed to enhance aerodynamic performance. These methods include the application of a sinusoidal surface [3], the use of air jets [4], the vortex generators [5], the implementation of split blades [6], and the combination of airfoils with vortex generators [7] on their surface and microcylinders [8].…”
Section: Introductionmentioning
confidence: 99%
“…The impact of microcylinders is most often tested at large rake angles of 16-23 • , as these angles generate boundary layers that are influenced by strong pressure gradients [9]. The addition of microcylinders delays flow detachment [8]. An important factor influencing the effectiveness of microcylinder additions is their location relative to the airfoil.…”
Section: Introductionmentioning
confidence: 99%