Optimal design of drag reduction oscillators by considering drillstring fatigue and hydraulic loss in sliding drilling

Author(s):  
Xiaolei Shi ◽  
Wenjun Huang ◽  
Deli Gao ◽  
Na Zhu
2013 ◽  
Vol 135 (11) ◽  
Author(s):  
Seong-Ho Seo ◽  
Chung-Do Nam ◽  
Jung-Young Han ◽  
Cheol-Hyun Hong

In this study, we used the Taguchi method to derive the optimal design parameters for the grooves formed on the upper surface of a circular cylinder. Using the derived values of the optimal design parameters, we created grooves on diphycercal the surfaces of a circular cylinder and analyzed the wake flow and the boundary-layer flow of the circular cylinder. The streamwise time mean velocity and turbulence intensity of the wake flow field were used as the characteristics. Based on these characteristics, the optimal design parameter values were selected: n = 3, k = 1.0 mm (k/d = 2.5%), and θ = 60 deg. When the grooved cylinder was used, the streamwise time mean velocity in the wake of the cylinder showed 12.3% recovery, the wake width was reduced by 18.4% compared to the results from the smooth cylinder and we had 28.2% drag reduction from that of smooth cylinder. Also, the flow on the smooth cylinder separated at around 82 deg but the flow separation on a grooved cylinder appeared beyond 90 deg, that reducing the drag.


2013 ◽  
Vol 404 ◽  
pp. 188-193
Author(s):  
Jing Chen ◽  
Tao Song ◽  
Deng Feng Wang

The drag reduction characteristic of air deflector of a heavy-duty vehicle is examined through CFD simulations and wind tunnel test in this paper. The CFD model of the truck is built using the FLUENT software and the simulation results are compared with the wind tunnel test data to verify the accuracy of simulation model. An air deflector is designed for this truck, A design of experiments approach was chosen as an efficient technique to optimize the design parameter and match with the truck to obtain the optimal drag reduction performance.


ICPTT 2012 ◽  
2012 ◽  
Author(s):  
Zhiqiang Zhao ◽  
Kun Yin ◽  
Lina Cao ◽  
Yongguang Zhang

2014 ◽  
Vol 602-605 ◽  
pp. 295-298 ◽  
Author(s):  
Xiao Lei Liu ◽  
Xue Wei Liu ◽  
Li Min Song ◽  
Dun Jin ◽  
Yuan Kai Li

In this paper, the international common CFD software were installed on the flat three-dimensional optimal design wing tip and winglet wing for three-dimensional simulation, and use the results post-processing software post-processing.


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