Many flight and icing conditions should be considered in order to design an efficient ice protection system to prevent ice accretion on the aircraft surface. The anti-icing heat load is the basic knowledge for the des...Many flight and icing conditions should be considered in order to design an efficient ice protection system to prevent ice accretion on the aircraft surface. The anti-icing heat load is the basic knowledge for the design of a thermal anti-icing system. In order to help the design of the thermal anti-icing system and save the design time, a fast and efficiency method for prediction the anti-icing heat load is investigated. The computation fluid dynamics (CFD) solver and the Messinger model are applied to obtain the snapshots. Examples for the calculation of the anti-icing heat load using the proper orthogonal decomposition (POD) method are presented and compared with the CFD simulation results. It is shown that the heat loads predicted by POD method are in agreement with the CFD computation results. Moreover, it is obviously to see that the POD method is time-saving and can meet the requirement of real-time prediction.展开更多
In this paper,we investigate a class of factorisable IC quasi-adequate semigroups,so-called,factorisable IC quasi-adequate semigroups of type-（H,I）.Some characterizations of factorisable IC quasi-adequate semigroups...In this paper,we investigate a class of factorisable IC quasi-adequate semigroups,so-called,factorisable IC quasi-adequate semigroups of type-（H,I）.Some characterizations of factorisable IC quasi-adequate semigroups of type-（H,I） are obtained.In particular,we prove that any IC quasi-adequate semigroup has a factorisable IC quasi-adequate subsemigroups of type-（H,I） and a band of cancellative monoids.展开更多
利用PIV技术在一台基于直喷汽油机(gasoline direct injection,GDI)改造的光学发动机上测量了缸内滚流运动,通过进气道入口处翻板和进气道内挡板改变缸内滚流比,并利用本征正交分解(POD)方法将流场分解为平均流场、拟序流场、过渡流场...利用PIV技术在一台基于直喷汽油机(gasoline direct injection,GDI)改造的光学发动机上测量了缸内滚流运动,通过进气道入口处翻板和进气道内挡板改变缸内滚流比,并利用本征正交分解(POD)方法将流场分解为平均流场、拟序流场、过渡流场和湍流流场,分析滚流运动对气流循环变动的影响。试验结果表明:翻板和挡板的组合能有效改变流场结构,使GDI汽油机缸内形成大尺度的单一滚流,滚流比提高近三倍。通过本征正交分解分析发现,拟序流场中拟序结构涡团的变动是缸内气流循环变动的主要来源。大尺度强滚流使平均流场占能比例大幅提升达30%,减少了能量向拟序流场的传递,使拟序流场循环变动降低近50%,从而抑制了缸内气流运动整体的循环变动。展开更多
The existence conditions of globally proper efficient points and a useful property of ic- cone-convexlike set-valued maps are obtained. Under the assumption of the ic-cone-convexlikeness, the optimality conditions for...The existence conditions of globally proper efficient points and a useful property of ic- cone-convexlike set-valued maps are obtained. Under the assumption of the ic-cone-convexlikeness, the optimality conditions for globally proper efficient solutions are established in terms of Lagrange multipliers. The new concept of globally proper saddle-point for an appropriate set-valued Lagrange map is introduced and used to characterize the globally proper efficient solutions. The results which are obtained in this paper are proven under the conditions that the ordering cone need not to have a nonempty interior.展开更多
文摘Many flight and icing conditions should be considered in order to design an efficient ice protection system to prevent ice accretion on the aircraft surface. The anti-icing heat load is the basic knowledge for the design of a thermal anti-icing system. In order to help the design of the thermal anti-icing system and save the design time, a fast and efficiency method for prediction the anti-icing heat load is investigated. The computation fluid dynamics (CFD) solver and the Messinger model are applied to obtain the snapshots. Examples for the calculation of the anti-icing heat load using the proper orthogonal decomposition (POD) method are presented and compared with the CFD simulation results. It is shown that the heat loads predicted by POD method are in agreement with the CFD computation results. Moreover, it is obviously to see that the POD method is time-saving and can meet the requirement of real-time prediction.
基金Supported by the NSF of Jiangxi Province(0511037)
文摘In this paper,we investigate a class of factorisable IC quasi-adequate semigroups,so-called,factorisable IC quasi-adequate semigroups of type-（H,I）.Some characterizations of factorisable IC quasi-adequate semigroups of type-（H,I） are obtained.In particular,we prove that any IC quasi-adequate semigroup has a factorisable IC quasi-adequate subsemigroups of type-（H,I） and a band of cancellative monoids.
基金supported in part by the National Natural Science Foundation of China(Nos.12172372,12132019)the National Major Science and Technology Projects(No.J2019-III-0010-0054).
文摘掌握结冰云雾参数的分布对于飞机结冰分析具有重要意义。为了获得这些参数,传统的高保真数值模拟技术计算效率低,难以应用于需要实时评估结冰的工程场景。为了克服这一困难,通过本征正交分解(Proper orthogonal decomposion,POD)方法与Kriging技术相结合,提出了一种非侵入式结冰云雾参数计算代理模型。该模型以4个飞行参数和2个云参数作为输入变量,模型输出为液体水含量(Liquid water content,LWC)和液滴收集系数。采用准三维NACA0012翼型验证了模型的准确性和计算效率。4个测试案例的数值结果表明:POD_Kriging模型准确、有效。相比于经典的FENSAP‐ICE软件,所开发的代理模型能够更有效的得到结冰云雾场。
文摘利用PIV技术在一台基于直喷汽油机(gasoline direct injection,GDI)改造的光学发动机上测量了缸内滚流运动,通过进气道入口处翻板和进气道内挡板改变缸内滚流比,并利用本征正交分解(POD)方法将流场分解为平均流场、拟序流场、过渡流场和湍流流场,分析滚流运动对气流循环变动的影响。试验结果表明:翻板和挡板的组合能有效改变流场结构,使GDI汽油机缸内形成大尺度的单一滚流,滚流比提高近三倍。通过本征正交分解分析发现,拟序流场中拟序结构涡团的变动是缸内气流循环变动的主要来源。大尺度强滚流使平均流场占能比例大幅提升达30%,减少了能量向拟序流场的传递,使拟序流场循环变动降低近50%,从而抑制了缸内气流运动整体的循环变动。
基金Supported by Natural Science Foundation of Ningxia (No.NZ0959)Natural Science Foundation of the State Ethnic Affairs Commission of PRC (No.09BF06)Natural Science Foundation for the Youth (No.10901004)
文摘The existence conditions of globally proper efficient points and a useful property of ic- cone-convexlike set-valued maps are obtained. Under the assumption of the ic-cone-convexlikeness, the optimality conditions for globally proper efficient solutions are established in terms of Lagrange multipliers. The new concept of globally proper saddle-point for an appropriate set-valued Lagrange map is introduced and used to characterize the globally proper efficient solutions. The results which are obtained in this paper are proven under the conditions that the ordering cone need not to have a nonempty interior.
