Throughout this paper,D=（d<sub>1</sub>,d<sub>2</sub>,...,d<sub>n</sub>）denote a sequence of nonnegative inte-gers.We let（?）（D）denote the class of all graphs with degree sequen...Throughout this paper,D=（d<sub>1</sub>,d<sub>2</sub>,...,d<sub>n</sub>）denote a sequence of nonnegative inte-gers.We let（?）（D）denote the class of all graphs with degree sequence D,or equally,theclass of all symmetric（0,1）--matrices with trace 0 and row sum vector D.The structure matrix S=S（D） of D is a matrix of order n+1,whose entries展开更多
The authors previously introduced a semi-empirical formula that enabled fast estimation of the added resistance of ships in head waves, and in this study the formula is further refined for easy use in engineering appl...The authors previously introduced a semi-empirical formula that enabled fast estimation of the added resistance of ships in head waves, and in this study the formula is further refined for easy use in engineering applications. It includes an alternative ship draft correction coefficient, which better accounts for the wave pressure decay with ship’s draft. In addition, it only uses the speed and main characteristics of the ship and wave environment as input, and has been simplified to the extent that it can be readily processed using a pocket calculator. Extensive validations are conducted for different ship types at low to moderate speeds in various typical irregular sea conditions, and encouraging results are obtained. This relevant and topical research lies within the framework of the recent IMO MEPC.232（65） （2013） EEDI guidelines for estimating the minimum powering of ships in adverse weather conditions, which specify for the use of simple methods in current Level 2 assessment within engineering applications.Keywords： added resistance, minimum power, IMO regulation, EEDI regulation, weather coefficient, semi-empirical formulas, ships, head waves展开更多
Our purpose is twofold: to present a prototypical example of the conditioning technique to obtain the best estimator of a parameter and to show that th</span><span style="font-family:Verdana;">is...Our purpose is twofold: to present a prototypical example of the conditioning technique to obtain the best estimator of a parameter and to show that th</span><span style="font-family:Verdana;">is technique resides in the structure of an inner product space. Th</span><span style="font-family:Verdana;">e technique uses conditioning </span></span><span style="font-family:Verdana;">of</span><span style="font-family:Verdana;"> an unbiased estimator </span><span style="font-family:Verdana;">on</span><span style="font-family:Verdana;"> a sufficient statistic. This procedure is founded upon the conditional variance formula, which leads to an inner product space and a geometric interpretation. The example clearly illustrates the dependence on the sampling methodology. These advantages show the power and centrality of this process.展开更多
航空发动机对尺寸有严格限制,甩油盘直径越大,雾化效果越好。针对甩油盘在发动机启动、慢车及高海拔地区工作时雾化性能不足,对甩油盘的最小适用直径Dmin进行了理论研究。甩油盘在液柱破碎模式时雾化性能最好,研究得到了各转速下甩油盘...航空发动机对尺寸有严格限制,甩油盘直径越大,雾化效果越好。针对甩油盘在发动机启动、慢车及高海拔地区工作时雾化性能不足,对甩油盘的最小适用直径Dmin进行了理论研究。甩油盘在液柱破碎模式时雾化性能最好,研究得到了各转速下甩油盘处于液柱破碎模式时燃油流量的计算方法。不同流量对应的液雾索特尔平均直径(Sauter Mean Diameter, SMD)不同,根据燃油流量计算得到甩油盘液雾SMD的范围,并由此推导出满足发动机启动、慢车状态要求的甩油盘最小适用直径Dmin的计算公式。高海拔对甩油盘雾化有不利影响,研究得到了海拔H处,甩油盘最小适用直径DHmin的计算公式。某型发动机启动转速为6000r/min,慢车转速为20000r/min,当燃油为航空煤油RP-3时,经理论分析,得到地面甩油盘直径应大于7.77cm;高海拔4000m处,甩油盘直径应大于9.49cm。展开更多
基金Supported by National Natural Science Foundation of China(No.19971086)
文摘Throughout this paper,D=（d<sub>1</sub>,d<sub>2</sub>,...,d<sub>n</sub>）denote a sequence of nonnegative inte-gers.We let（?）（D）denote the class of all graphs with degree sequence D,or equally,theclass of all symmetric（0,1）--matrices with trace 0 and row sum vector D.The structure matrix S=S（D） of D is a matrix of order n+1,whose entries
基金Partly Supported by the Collaborative Project SHOPERA under Grant Agreement No.605221
文摘The authors previously introduced a semi-empirical formula that enabled fast estimation of the added resistance of ships in head waves, and in this study the formula is further refined for easy use in engineering applications. It includes an alternative ship draft correction coefficient, which better accounts for the wave pressure decay with ship’s draft. In addition, it only uses the speed and main characteristics of the ship and wave environment as input, and has been simplified to the extent that it can be readily processed using a pocket calculator. Extensive validations are conducted for different ship types at low to moderate speeds in various typical irregular sea conditions, and encouraging results are obtained. This relevant and topical research lies within the framework of the recent IMO MEPC.232（65） （2013） EEDI guidelines for estimating the minimum powering of ships in adverse weather conditions, which specify for the use of simple methods in current Level 2 assessment within engineering applications.Keywords： added resistance, minimum power, IMO regulation, EEDI regulation, weather coefficient, semi-empirical formulas, ships, head waves
文摘Our purpose is twofold: to present a prototypical example of the conditioning technique to obtain the best estimator of a parameter and to show that th</span><span style="font-family:Verdana;">is technique resides in the structure of an inner product space. Th</span><span style="font-family:Verdana;">e technique uses conditioning </span></span><span style="font-family:Verdana;">of</span><span style="font-family:Verdana;"> an unbiased estimator </span><span style="font-family:Verdana;">on</span><span style="font-family:Verdana;"> a sufficient statistic. This procedure is founded upon the conditional variance formula, which leads to an inner product space and a geometric interpretation. The example clearly illustrates the dependence on the sampling methodology. These advantages show the power and centrality of this process.
文摘航空发动机对尺寸有严格限制,甩油盘直径越大,雾化效果越好。针对甩油盘在发动机启动、慢车及高海拔地区工作时雾化性能不足,对甩油盘的最小适用直径Dmin进行了理论研究。甩油盘在液柱破碎模式时雾化性能最好,研究得到了各转速下甩油盘处于液柱破碎模式时燃油流量的计算方法。不同流量对应的液雾索特尔平均直径(Sauter Mean Diameter, SMD)不同,根据燃油流量计算得到甩油盘液雾SMD的范围,并由此推导出满足发动机启动、慢车状态要求的甩油盘最小适用直径Dmin的计算公式。高海拔对甩油盘雾化有不利影响,研究得到了海拔H处,甩油盘最小适用直径DHmin的计算公式。某型发动机启动转速为6000r/min,慢车转速为20000r/min,当燃油为航空煤油RP-3时,经理论分析,得到地面甩油盘直径应大于7.77cm;高海拔4000m处,甩油盘直径应大于9.49cm。
