Amsha, K. A., Craft, T. J., & Iacovides, H. (2017). Computational modelling of the flow and heat transfer in dimpled channels
. The Aeronautical Journal, 121(1242), 1066–1086.
https://doi.org/10.1017/aer.2017.68
Cao, Z., Gao, X., Zhang, X., Zhang, F., & Liu, B. (2021). Influence of endwall air injection with discrete holes on corner separation of a compressor cascade.
Journal of Thermal Science,
30(5), 1684-1704.
https://link.springer.com/article/10.1007/s11630-021-1513-5
Casey, J., King, P., & Sondergaard, R. (2004).
Parameterization of boundary layer control dimples on a low pressure turbine blade. 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
https://arc.aiaa.org/doi/abs/10.2514/6.2004-3570
Chen, H., Liu, H., Zhang, D., & Li, L. (2017, June).
Vortex structures for highly-loaded subsonic compressor cascades with slot injection. Turbo Expo: Power for Land, Sea, and Air, American Society of Mechanical Engineers.
https://doi.org/10.1115/GT2017-63781
Chen, Y., Yang, L., & Zhong, J. (2019). Numerical study on end wall fence with varying geometrical parameters in a highly-loaded compressor cascade.
Aerospace Science and Technology. 94, 105390.
https://doi.org/10.1016/j.ast.2019.105390
Chishty, M. A., Parvez, K., Ahmed, S., Hamdani, H. R., & Mushtaq, A. (2011, January).
Transition prediction in low pressure turbine (LPT) using gamma theta model and passive control of separation. ASME International Mechanical Engineering Congress and Exposition.
https://doi.org/10.1115/IMECE2011-62148
Chung, K. M., Su, K. C., & Chang, K. C. (2021). The Effect of vortex generators on shock-induced boundary layer separation in a transonic convex-corner flow.
Aerospace.
8, 157.
https://doi.org/10.3390/aerospace8060157
D'Alessandro, V., Clementi, G., Giammichele, L., & Ricci, R. (2019). Assessment of the dimples as passive boundary layer control technique for laminar airfoils operating at wind turbine blades root region typical Reynolds numbers.
Energy,
170, 102-111.
https://doi.org/10.1016/j.energy.2018.12.070
Jeong, H., & Song, S. J. (2021). Influence of surface roughness on the flat-plate boundary layer transition under a high-lift airfoil pressure gradient and low freestream turbulence.
American Society of Mechanical Engineers Digital Collection, GT2021-59192.
https://doi.org/10.1115/GT2021-59192
Lan, J., Xie, Y., & Zhang, D. (2011). Effect of leading edge boundary layer thickness on dimple flow structure and separation control.
Journal of Mechanical Science and Technology,
25, 3243-3251.
https://doi.org/10.1007/s12206-011-0823-z
Liang, T., Liu, B., & Spence, S. (2021). Effect of boundary layer suction on the corner separation in a highly loaded axial compressor cascade. American Society of Mechanical Engineers Digital Collection. 143(6), 061002. https://doi.org/10.1115/GT2020-14566
Liesner, K., & Meyer, R. (2013).
Evaluation of passive and active secondary flow control in a high speed compressor cascade with different measurement techniques. New Results in Numerical and Experimental Fluid Mechanics VIII: Contributions to the 17th STAB/DGLR Symposium Berlin, Germany 2010, Springer Berlin Heidelberg.
https://doi.org/10.1007/978-3-642-35680-3_16
Lu, H. W., Yang, Y., Guo, S., Huang, Y. X., Wang, H., & Zhong, J. J. (2018a). The effect of dimpled surface on loss reduction and vortices in a highly loaded compressor cascade.
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,
232(2), 374-387.
https://doi.org/10.1177/0954410017728976
Lu, H. W., Yang, Y., Guo, S., Huang, Y. X., Wang, H., & Zhong, J. J. (2018b). Flow control in linear compressor cascades by inclusion of suction side dimples at varying locations.
Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy,
232(6), 706-721.
https://doi.org/10.1177/0957650917752276
Lu, H., Yang, Y., Guo, S., Pang, W., Yang, F., & Zhong, J. (2019). Control of corner separation via dimpled surface for a highly loaded compressor cascade under different inlet Mach number.
Aerospace Science and Technology,
85, 48-60.
https://doi.org/10.1016/j.ast.2018.11.054
Rouser, K. P. (2002).
Use of dimples to suppress boundary layer separation on a low pressure turbine blade [Master’s thesis, Department of Aeronautics and Astronautics].
https://scholar.afit.edu/etd/4139
Tian, L., Li, Z., Jin, E., Ke, Q., Dong, S., & Ma, Y. (2015). Improved flow performance of a centrifugal compressor based on pit formation on the notum of the whirligig beetle (Gyrinidae Latreille).
Advances in Mechanical Engineering,
7(7), 16878140-15591736.
https://doi.org/10.1177/1687814015591736
Wang, L., Lu, H., Tian, Z., Yang, Y., Guo, S., Wang, H., & Kong, X. (2022). Numerical study of the ratio of depth-to-print diameter on the performance and flow characteristics for a dimpled, highly loaded compressor cascade.
Aerospace,
9(8), 422.
https://doi.org/10.3390/aerospace9080422
Wang. L., Lu, H., Guo, S., Pang, W., Song, H., & Yang, Y. (2020). Influence of arrangement of dimples on highly loaded compressor cascade. Journal of Engineering Thermophilic, 41(11), 2677-2686.
Xu, W., Sun, P., & Yang, G. (2021). Effect of the bionic chamber position on the aerodynamic performance in a transonic compressor cascade.
Aerospace Science and Technology,
119, 107106.
https://doi.org/10.1016/j.ast.2021.107106
Zhang, H., Wu, Y., Li, Y., & Lu, H. (2015). Experimental investigation on a high subsonic compressor cascade flow.
Chinese Journal of Aeronautics,
28(4), 1034-1043.
https://doi.org/10.1016/j.cja.2015.06.019
Zhang, H., Yu, X., Liu, B., Wu, Y., & Li, Y. (2017). Control of corner separation with plasma actuation in a high-speed compressor cascade.
Applied Sciences,
7(5), 465.
https://doi.org/10.3390/app7050465
Zhao, Y., Lu, H., & Sun, Y. (2016). Experimental studies of dimpled surface effect on the performance of linear cascade under different incidence angles.
Procedia CIRP,
56, 137-142.
https://doi.org/10.1016/j.procir.2016.10.043
Zinchenko, I. M., Skoryk, A., & Parafejnik, V. (2016). On the effect of spherical dimples at diffuser vane surface on performance of centrifugal compressor.
NTU "KhPI" Bulletin: Power and Heat Engineering Processes and Equipment, (9), 37-43.
https://doi.org/10.20998/2078774X.2016.09.05