喷流干扰效应的快速计算方法

给出了一种快速计算火箭发动机喷流流场的方法,并在此基础上发展了一种计算喷流与物面间干扰流场及飞行器气动特性的工程计算方法。该方法不仅考虑了喷流与物面的碰撞,还考虑了有攻角下自由来流与喷流间的相互干扰。计算结果表明,该方法对飞行器初步设计是十分有用的工具     

分布式结点自组织时分多址算法

提出了一种分布式结点自组织时分多址算法,并论证了算法的正确性和功效。     

火炮刹车性能的全静态检测

本又分析了影响火炮刹车性能的问题所在,并提出一种新的检测方法,使火炮在全静态条件下,检测各项静态参数、评价刹车系统的质量。     

带有先验分布的Bayes统计抽样方案费用评价模型

以往在评价和比较几个统计抽样方案时,多从比较分析两种风险率入手,由于这种方法的局限性,往往不能得出满意的结论。本文利用Bayes方法,在给出先验分布及有关损失函数的条件下,从各种抽样方案的平均总损失入手比较几个可选方案的优良性。本文提供的与二项分布相对应的算法具有一般意义。示例所得结果也是令人满意的。     

A finite-range distribution of failure times

Properties of a finite-range failure-time distribution, that includes the exponential as a particular case, have been studied. The distribution is IFR when the shape parameter exceeds unity, but is IFRA always. For a given value of the shape parameter, the distribution is NBUE over a segment of its range. Estimators of parameters have been derived. Distributions of two-component series, parallel, and standby system lives have also been worked out.     

Extrapolation of the mean lifetime of a large population from its preliminary survival history

A large population of independent identical units having finite mean lifetime T is observed. From the history A(y) of cumulative arrivals and the history B(y) of cumulative removals in the interval 0 ≦ y ≦ τ one must predict at time τ the desired T . Two lifetime predictors X(τ) and Y(τ) and related simple predictors obtained from A(y) and B(y) are shown to converge to T with a rate of convergence dependent on the structure of the failure rate function of the units. This dependence is studied theoretically and numerically.