4.7 Article

Analytic Solution of Optimal Aspect Ratio of Bionic Transverse V-Groove for Drag Reduction Based on Vorticity Kinetics

Journal

AEROSPACE
Volume 9, Issue 12, Pages -

Publisher

MDPI
DOI: 10.3390/aerospace9120749

Keywords

transverse groove; drag reduction; aspect ratio; boundary vortex stability; LES

Funding

  1. National Natural Science Foundation of China
  2. National Science and Technology Major Project
  3. [52176032]
  4. [2017-?-0005-0016]

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Previous studies have found that the aspect ratio (AR) of a transverse groove significantly affects the stability of the boundary vortex and the rate of drag reduction. However, there is currently no theoretical model that describes the relationship between AR and the stability of the boundary vortex, making it difficult to develop a method to determine the optimal AR. In this study, an image vortex model is used to describe the velocity potential of the groove sidewalls, establishing the relationship between AR and induced velocity. The velocity profile of the migration flow is obtained by decomposing the total velocity inside the groove, allowing for the relationship between AR and migration velocity to be established. An analytical solution for the optimal AR is derived based on the kinematic condition for boundary vortex stability, and the motion forms of the boundary vortex at other ARs are discussed. The stability of the boundary vortex at the optimal AR and the corresponding drag reduction rate are verified through large eddy simulations. At other ARs, the motion forms of the boundary vortex are characterized by vortex shedding and vortex sloshing, with corresponding drag reduction rates smaller than those for vortex stability.
Previous studies have implied that the AR (aspect ratio) of the transverse groove significantly affects the stability of the boundary vortex within the groove and thus drives the variation in the drag-reduction rate. However, there is no theoretical model describing the relationship between the AR and the stability of the boundary vortex, resulting in difficulty in developing a forward method to obtain the optimum AR. In this paper, the velocity potential of the groove sidewalls to the boundary vortex is innovatively described by an image vortex model, thus establishing the relationship between the AR and the induced velocity. Secondly, the velocity profile of the migration flow is obtained by decomposing the total velocity inside the groove, by which the relationship between the AR and the migration velocity is established. Finally, the analytical solution of the optimal AR (AR(opt) =2.15) is obtained based on the kinematic condition for boundary vortex stability, i.e., the induced velocity equals the migration velocity, and the forms of boundary vortex motion at other ARs are discussed. Furthermore, the stability of the boundary vortex at the optimal AR and the corresponding optimal drag-reduction rate are verified by the large eddy simulations method. At other ARs, the motion forms of the boundary vortex are characterized by vortex shedding and vortex sloshing, respectively, and the corresponding drag-reduction rates are smaller than those for vortex stability.

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