期刊文献+
共找到3篇文章
< 1 >
每页显示 20 50 100
Storage stability of SBS modified bitumen based on mixed-level orthogonal array design
1
作者 杨群 何文华 《Journal of Southeast University(English Edition)》 EI CAS 2012年第3期337-343,共7页
The styrene-butadiene-styrene(SBS) modified bitumens with different contents of SBS modifiers are stored in different conditions to study the storage stability of SBS modified bitumen.Mixed-level orthogonal array de... The styrene-butadiene-styrene(SBS) modified bitumens with different contents of SBS modifiers are stored in different conditions to study the storage stability of SBS modified bitumen.Mixed-level orthogonal array design(OAD) is used and factors such as SBS modifier content,storage time,storage temperature and container size are chosen in a mixed-level OAD with an OA16(31×44) matrix.Parameters like the separation softening point difference(the separation difference of the ring and ball softening point of the top and bottom samples) and the average softening point(the arithmetic mean of the softening points of the top and bottom samples) are proposed to evaluate the separation and the ageing of modified bitumen during storage in this experiment,respectively.The results reveal that the separation and the ageing during storage exhibit a complicated variation for storage temperature and time.The separation softening point difference decreases with the storage temperature rising from 20 to 120 ℃ and increases with the temperature exceeding 120 ℃,and the average softening point drops with the storage time being prolonged.Different storage conditions have various effects on the storage stability of SBS modified bitumen. 展开更多
关键词 storage stability mixed-level orthogonal array design separation softening point difference average softening point
下载PDF
Numerical simulation on influence of jet angle on jet's characteristics in flowing ambient fluid
2
作者 周丰 孙昭晨 梁书秀 《Journal of Harbin Institute of Technology(New Series)》 EI CAS 2008年第4期528-534,共7页
Based on the stress-algebraic model, the turbulent buoyant jet with variable density was studied by the relation between density and concentration. A simple expression for buoyancy coefficient was proposed. The govern... Based on the stress-algebraic model, the turbulent buoyant jet with variable density was studied by the relation between density and concentration. A simple expression for buoyancy coefficient was proposed. The governing equations of turbulent buoyant jet with variable density were closed by introducing the expression of β and the relation between density and concentration. Numerical results for the jet axis with density difference agree well with experimental ones. By finite volume method, the 2 - D vertical jet's flow field with different jet angles was studied. The analysis of the relation among the vortex center, the position of separation point and jet angles shows that the circumfluenee field is the largest when the jet angle is 90°. The area turbulent kinetic energy ka is proposed and the relationship between mixing intensity and jet angles is analyzed based on it. Results show that the jet angle of is the optimum condition for jet water mixing with environment water;and the reduced rate of difference between the centerline density of jet and the density of ambient water is the largest at the jet angle of 90°. 展开更多
关键词 jet angle stress-algebraic model with variable density vortex center point separation point areaturbulent kinetic energy
下载PDF
Numerical Tools for the Control of the Unsteady Heating of an Airfoil
3
作者 Franqoise Masson Francisco Chinesta +4 位作者 Adrien Leygue Chady Ghnatios Elias Cueto Laurent Dala Craig Law 《Journal of Mechanics Engineering and Automation》 2013年第6期339-351,共13页
This paper concerns the real time control of the boundary layer on an aircraft wing. This new approach consists in heating the surface in an unsteady regime using electrically resistant strips embedded in the wing ski... This paper concerns the real time control of the boundary layer on an aircraft wing. This new approach consists in heating the surface in an unsteady regime using electrically resistant strips embedded in the wing skin. The control of the boundary layer's separation and transition point will provide a reduction in friction drag, and hence a reduction in fuel consumption. This new method consists in applying the required thermal power in the different strips in order to ensure the desired temperatures on the aircraft wing. We also have to determine the optimum size of these strips (length, width and distance between two strips). This implies finding the best mathematical model corresponding to the physics enabling us to facilitate the calculation for any type of material used for the wings. Secondly, the heating being unsteady, and, as during a flight the flow conditions or the ambient temperatures vary, the thermal power needed changes and must be chosen as fast as possible in order to ensure optimal operating conditions. 展开更多
关键词 Model reduction PGD (proper generalized decomposition) heating of an airfoil boundary layers laminar-turbulenttransition and separation point friction drag unsteady heating.
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部