Experimental Study of a Densely Perforated Plate Bending

Author(s):  
A. M. Popov ◽  
V. B. Zinoviev ◽  
S. I. Gerasimov ◽  
L. A. Spodareva
2018 ◽  
Vol 43 (17) ◽  
pp. 8524-8533 ◽  
Author(s):  
Quan Li ◽  
Xuxu Sun ◽  
Shouxiang Lu ◽  
Zhi Zhang ◽  
Xing Wang ◽  
...  

Author(s):  
A’rasy Fahruddin

HHO merupakan gas hasil elektrolisa air yang dapat digunakan sebagai bahan bakar tambahan pada motor bakar. Penelitian ini bertujuan mengetahui karakteristik generator HHO menggunakan elektroda pelat berlubang. Elektroda yang dipakai berupa pelat aluminium dengan ukuran 60 x 60 x 0.5 mm3 dengan variasi tanpa lubang, 4 lubang, 6 lubang, dan 9 lubang. Masing-masing lubang berdiameter 4 mm. Variasi tegangan input 3,5; 6; 7,5; 9 Volt. Karakteristik yang diuji meliputi daya input, debit, dan efisiensi generator HHO. Hasil yang didapatkan dari penelitian ini adalah bahwa debit gas HHO yang terbesar dihasilkan dengan elektroda 9 lubang yaitu sebesar 5,77 cc/min dengan daya input 4,59 Watt. Sedangkan efisiensi generator tertinggi juga dihasilkan dengan elektroda 9 lubang yang mampu mencapai efisiensi 63,16 % dengan daya input 0,52 Watt.


Author(s):  
Himanshu Tyagi ◽  
Rui Liu ◽  
David S.-K. Ting ◽  
Clifton R. Johnston

The study of vortex shedding from a sphere assumes an important role because of its relevance to numerous aerodynamic and hydrodynamic applications. Parameters such as coefficient of drag and static pressure distribution are largely influenced by vortex shedding, and it is found by past studies that the freestream turbulence can interact and alter the vortex formation and shedding drastically. Most of these studies, however, were conducted in the low Reynolds number regime and the vortex shedding results had been described only qualitatively. To better understand the aerodynamics of a sphere in turbulent flow, an experimental study was initiated in a low speed wind tunnel to quantify the vortex shedding characteristics. The Reynolds number of the flow, based on the diameter of the sphere (d), was set at 3.3 × 104, 5 × 104 and 6.6 × 104 by varying the mean flow velocity. The sphere was placed at 20D (= 7.5d) downstream from a perforated plate, where D = 37.5 mm is the size of the holes in the perforated plate, uniquely designed for generating near-isotropic turbulence. Hot-wire measurements were taken at 10D (= 3.75d), 20D (= 7.5d) and 30D (= 11.25d) downstream of the sphere in absence and presence of the perforated plate. The vortex shedding frequency was deduced from the instantaneous flow velocity data.


Fuel ◽  
2020 ◽  
Vol 263 ◽  
pp. 116733 ◽  
Author(s):  
Yang Wan ◽  
Changjian Wang ◽  
Quan Li ◽  
Xinjiao Luo

2011 ◽  
Vol 4 (4) ◽  
pp. 223-233 ◽  
Author(s):  
Chingiz Rahimov ◽  
Ismayil Farzaliyev

The reconstruction of acquired mandibular defects due to ablative tumor surgery or traumatic injuries is still challenging. The gold standard in such treatment is application of reconstructive titanium plates, which should be contoured and adapted to the defect as much as possible because of their influence on postoperative functional and esthetic results. Traditionally, plate bending is achieved by trial and error intraoperatively. Use of stereolitography (STL) models potentially could reduce the risk of incorrect contouring as well as operating time. On the other hand, fabrication of STL is time-consuming and costly. However, we found only one experimental study dedicating to virtual plate bending in the literature. The aim of this article was to demonstrate clinical application of a method of virtual bending of reconstructive plate for mandibular defect bridging. No significant complications occurred, and satisfactory functional and esthetic results were achieved in all cases. We found this technique precise and applicable in cases of reconstruction of mandibular defects.


Energy ◽  
2017 ◽  
Vol 122 ◽  
pp. 159-167 ◽  
Author(s):  
Sherif S. Rashwan ◽  
Abdelmaged H. Ibrahim ◽  
Tharwat W. Abou-Arab ◽  
Medhat A. Nemitallah ◽  
Mohamed A. Habib

2016 ◽  
Vol 15 (4) ◽  
pp. 382-387 ◽  
Author(s):  
Sayed Mohammad Reza Hodaei ◽  
Mohammad Reza Chamani ◽  
Mohammad Navid Moghim ◽  
Shahriar Mansoorzadeh ◽  
Abdoreza Kabiri-Samani

2015 ◽  
Vol 35 (2) ◽  
pp. 1973-1979 ◽  
Author(s):  
Hui Qin ◽  
John H.S. Lee ◽  
Zhenguo Wang ◽  
Fengchen Zhuang

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